The University of Queensland

Free piston shock tunnels HEG, HIEST, T4 and T5

Hannemann, Klaus, Itoh, Katsuhiro, Mee, David J. and Hornung, Hans G. (2016). Free piston shock tunnels HEG, HIEST, T4 and T5. Experimental methods of shock wave research. (pp. 181-264) edited by Hans Grönig, Yasuyuki Horie and Kazuyoshi Takayama. London, United Kingdom: Springer International Publishing. doi: 10.1007/978-3-319-23745-9_7

Noise Generated in a Scramjet Combustor

Ananthapadmanaban, Ramprakash, McIntyre, Timothy J., Wheatley, Vincent and Mee, David J. (2024). Noise Generated in a Scramjet Combustor. Journal of Spacecraft and Rockets, 1-13. doi: 10.2514/1.a35779

Heat-transfer gauge arrays for identifying spot initiation in hypersonic transitional boundary layers

Mee, David J., Raghunath, Sreekanth and McGilvray, Matthew (2023). Heat-transfer gauge arrays for identifying spot initiation in hypersonic transitional boundary layers. Journal of Spacecraft and Rockets, 60 (5), 1-8. doi: 10.2514/1.a35662

Optimum combination of diesel and concentrating solar in remote area power generation using supercritical CO2 turbines

Lee, Sangkyoung, Mee, David J., Guan, Zhigiang and Gurgenci, Hal (2023). Optimum combination of diesel and concentrating solar in remote area power generation using supercritical CO2 turbines. Energy Conversion and Management, 278 116714, 116714. doi: 10.1016/j.enconman.2023.116714

Off-Design Performance Prediction of Supercritical Co2 Radial Inflow Turbines

Lee, Sankyoung, Mee, David J., Guan, Zhigiang and Gurgenci, Hal (2022). Off-Design Performance Prediction of Supercritical Co2 Radial Inflow Turbines. SSRN Electronic Journal, 1-28. doi: 10.2139/ssrn.4166502

Heat transfer measurements in an expansion tube using infrared thermography

Ramesh, Ranjini, Morgan, Richard G. and Mee, David J. (2022). Heat transfer measurements in an expansion tube using infrared thermography. AIAA Journal, 60 (2), 883-891. doi: 10.2514/1.J059919

Part-load performance prediction model for supercritical CO2 radial inflow turbines

Lee, Sangkyoung, Yaganegi, Grant, Mee, David J., Guan, Zhigiang and Gurgenci, Hal (2021). Part-load performance prediction model for supercritical CO2 radial inflow turbines. Energy Conversion and Management, 235 113964, 1-11. doi: 10.1016/j.enconman.2021.113964

Magnetohydrodynamic drag force measurements in an expansion tunnel using a stress wave force balance

Smith, Daniel R., Gildfind, David E., Mee, David J., James, Christopher M. and Allsop, Barry V. (2020). Magnetohydrodynamic drag force measurements in an expansion tunnel using a stress wave force balance. Experiments in Fluids, 61 (8) 180. doi: 10.1007/s00348-020-03015-4

Magnetohydrodynamic drag force measurements in expansion tunnels using an accelerometer-based force balance

Smith, Daniel R., Gildfind, David E., McIntyre, Timothy J., Mee, David J., James, Christopher M. and Andrianatos, Andreas (2019). Magnetohydrodynamic drag force measurements in expansion tunnels using an accelerometer-based force balance. Experiments in Fluids, 60 (12) 183. doi: 10.1007/s00348-019-2828-9

Estimating turbulent spot initiation rates from transition lengths in hypersonic boundary layers

Raghunath, Sreekanth, Mee, David and Narasimha, Roddam (2017). Estimating turbulent spot initiation rates from transition lengths in hypersonic boundary layers. AIAA Journal, 55 (11), 3640-3647. doi: 10.2514/1.J055502

Drag reduction by boundary-layer combustion: effects of flow disturbances from rectangular-to-elliptical-shape-transition inlets

Chan, Wilson Y. K., Mee, David J., Smart, Michael K. and Turner, James C. (2015). Drag reduction by boundary-layer combustion: effects of flow disturbances from rectangular-to-elliptical-shape-transition inlets. Journal of Propulsion and Power, 31 (5), 1256-1267. doi: 10.2514/1.B35335

Drag reduction by boundary-layer combustion: influence from disturbances typical of cross-stream fuel-injection

Chan, Wilson Y. K., Mee, David J., Smart, Michael K. and Turner, James C. (2015). Drag reduction by boundary-layer combustion: influence from disturbances typical of cross-stream fuel-injection. Journal of Propulsion and Power, 31 (5), 1486-1491. doi: 10.2514/1.B35665

Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions

Tanimizu, Katsuyoshi, Mee, David J., Stalker, Raymond J. and Jacobs, Peter A. (2013). Nozzle design study for a quasi-axisymmetric scramjet-powered vehicle at Mach 7.9 flight conditions. Shock Waves, 23 (5), 453-460. doi: 10.1007/s00193-013-0449-4

An experimental study on aerodynamic performance of turbine nozzle guide vanes with trailing-edge span-wise ejection

Aminossadati, S. M. and Mee, D. J. (2013). An experimental study on aerodynamic performance of turbine nozzle guide vanes with trailing-edge span-wise ejection. Journal of Turbomachinery, 135 (3) 031002, 031002.1-031002.12. doi: 10.1115/1.4006663

Suitability of the k-omega turbulence model for scramjet flowfield simulations

Chan, W. Y. K., Jacobs, P. A. and Mee, D. J. (2012). Suitability of the k-omega turbulence model for scramjet flowfield simulations. International Journal for Numerical Methods in Fluids, 70 (4), 493-514. doi: 10.1002/fld.2699

Nanoparticle-induced morphology and hydrophilicity of structured surfaces

Gao, Nan, Yan, Yuying, Chen, Xinyong and Mee, David J. (2012). Nanoparticle-induced morphology and hydrophilicity of structured surfaces. Langmuir, 28 (33), 12256-12265. doi: 10.1021/la302627n

Supersonic skin-friction drag with tangential wall slot fuel injection and combustion

Kirchhartz, Rainer M., Mee, David J. and Stalker, Raymond J. (2012). Supersonic skin-friction drag with tangential wall slot fuel injection and combustion. AIAA Journal, 50 (2), 313-324. doi: 10.2514/1.J051073

Numerical modelling of the self-heating process of a wet porous medium

Ejlali, A., Mee, D.J., Hooman, K. and Beamish, B.B. (2011). Numerical modelling of the self-heating process of a wet porous medium. International Journal of Heat and Mass Transfer, 54 (25-26), 5200-5206. doi: 10.1016/j.ijheatmasstransfer.2011.08.025

Superhydrophobic surfaces with hierarchical structure

Gao, N., Yan, Y. Y., Chen, X. Y. and Mee, D. J. (2011). Superhydrophobic surfaces with hierarchical structure. Materials Letters, 65 (19-20), 2902-2905. doi: 10.1016/j.matlet.2011.06.088

Thrust nozzle design study for a quasi-axisymmetric scramjet-powered vehicle

Tanimizu, K, Mee, DJ, Stalker, RJ and Jacobs, PA (2011). Thrust nozzle design study for a quasi-axisymmetric scramjet-powered vehicle. Journal of Propulsion and Power, 27 (1), 40-49. doi: 10.2514/1.48586

Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flows

Kirchhartz, Rainer M., Paull, Allan, Mee, David J. and Olivier, Herbert (2010). Self ignition of hydrogen-air mixtures with inclined porthole injection in supersonic flows. International Journal of Hypersonics, 1 (4), 199-208. doi: 10.1260/1759-3107.1.4.199

Attitude guidance for spinning vehicles with independent pitch and yaw control

Creagh, Michael and Mee, David (2010). Attitude guidance for spinning vehicles with independent pitch and yaw control. Journal of Guidance, Control and Dynamics, 33 (3), 915-922. doi: 10.2514/1.44430

Supersonic boundary-layer combustion: Effects of upstream entropy and shear-layer thickness

Kirchhartz, R. M., Mee, D. J., Stalker, R. J., Jacobs, P. A. and Smart, M. K. (2010). Supersonic boundary-layer combustion: Effects of upstream entropy and shear-layer thickness. Journal of Propulsion and Power, 26 (1), 57-66. doi: 10.2514/1.44485

Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: Theory and experiment

Tanimizu, K, Mee, DJ, Stalker, RJ and Jacobs, PA (2009). Drag force on quasi-axisymmetric scramjets at various flight Mach numbers: Theory and experiment. SHOCK WAVES, 19 (2), 83-93. doi: 10.1007/s00193-009-0194-x

Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow

Frost, Myles A., Gangurde, Dhananjay Y., Paull, Allan and Mee, David J. (2009). Boundary-layer separation due to combustion-induced pressure rise in a supersonic flow. AIAA Journal, 47 (4), 1050-1053. doi: 10.2514/1.40868

Effect of anti-scale agents on the solubility of CO2 in seawater at temperatures of 60 to 90oC and pressures of 1-2 bar

Al-Anezi, Khalid, Somerfield, Chris, Mee, David, Hankins, Nick and Hilal, Nidal (2008). Effect of anti-scale agents on the solubility of CO2 in seawater at temperatures of 60 to 90oC and pressures of 1-2 bar. Desalination, 227 (1-3), 46-56. doi: 10.1016/j.desal.2007.05.034

Parameters affecting the solubility of carbon dioxide in seawater at the conditions encountered in MSF desalination plants

Al-Anezi, Khalid, Somerfield, Chris, Mee, David and Hilal, Nidal (2008). Parameters affecting the solubility of carbon dioxide in seawater at the conditions encountered in MSF desalination plants. Desalination, 222 (1-3), 548-571. doi: 10.1016/j.desal.2007.01.128

New calibration technique for multiple-component stress wave force balances

Abdel-Jawad, Madhat M., Mee, David J. and Morgan, Richard G. (2007). New calibration technique for multiple-component stress wave force balances. Review of Scientific Instruments, 78 (6) 065101, 065101-1-065101-7. doi: 10.1063/1.2744235

Background oriented schlieren for flow visualisation in hypersonic impulse facilities

Ramanah, D., Raghunath, S., Mee, D. J., Rosgen, T. and Jacobs, P. A. (2007). Background oriented schlieren for flow visualisation in hypersonic impulse facilities. Shock Waves, 17 (1-2), 65-70. doi: 10.1007/s00193-007-0097-7

Boundary layers on a flat plate at suband superorbital speeds

Hayne, M.J., Mee, D.J., Gai, S.L. and McIntyre, T.J. (2007). Boundary layers on a flat plate at suband superorbital speeds. Journal of Thermophysics And Heat Transfer, 21 (4), 772-779. doi: 10.2514/1.26894

Reynolds analogy in high-enthalpy and high-Mach-number turbulent flows

Suraweera, M. V., Mee, D. J. and Stalker, R. J. (2006). Reynolds analogy in high-enthalpy and high-Mach-number turbulent flows. Aiaa Journal, 44 (4), 917-919. doi: 10.2514/1.18939

Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnel

Robinson, M. J., Mee, D. J. and Paull, A. (2006). Scramjet lift, thrust and pitching-moment characteristics measured in a shock tunnel. Journal Of Propulsion And Power, 22 (1), 85-95. doi: 10.2514/1.15978

Scramjets and Shock Tunnels: The Queensland Experience

Stalker, R. J., Paull, A., Mee, D. J., Morgan, R. G. and Jacobs, P. A. (2005). Scramjets and Shock Tunnels: The Queensland Experience. Progress in Aerospace Sciences, 41 (6), 471-513. doi: 10.1016/j.paerosci.2005.08.002

Dynamic force balances for short-duration hypersonic testing facilities

Sahoo, N., Suryavamshi, K., Reddy, K. P. J. and Mee, D. J. (2005). Dynamic force balances for short-duration hypersonic testing facilities. Experiments In Fluids, 38 (5), 606-614. doi: 10.1007/s00348-005-0932-5

Rarefied, Superorbital Flows in an Expansion Tube

Wheatley, Vincent, Chiu, Sam Hsieh-Hsiang, Jacobs, Peter A., Macrossan, Michael N., Mee, David J. and Morgan, Richard G. (2004). Rarefied, Superorbital Flows in an Expansion Tube. International Journal for Numerical Methods for Heat and Fluid Flow, 14 (4), 512-537. doi: 10.1108/09615530410532277

Dynamic Calibration of Force Balances for Impulse Hypersonic Facilities

Mee, D. J. (2003). Dynamic Calibration of Force Balances for Impulse Hypersonic Facilities. Shock Waves, 12 (6), 443-455. doi: 10.1007/s00193-003-0181-6

Heat transfer and flow behind a step in high enthalpy superorbital flow

Hayne, MJ, Mee, DJ, Morgan, RG, Gai, SL and McIntyre, TJ (2003). Heat transfer and flow behind a step in high enthalpy superorbital flow. Aeronautical Journal, 107 (1073), 435-442. doi: 10.1017/s0001924000130040

Techniques for detailed heat transfer measurements in cold supersonic blowdown tunnels using thermochromic liquid crystals

Mee, D. J., Chiu, H. S. and Ireland, P. T. (2002). Techniques for detailed heat transfer measurements in cold supersonic blowdown tunnels using thermochromic liquid crystals. International Journal of Heat And Mass Transfer, 45 (16), 3287-3297. doi: 10.1016/S0017-9310(02)00050-9

Thermochromic liquid crystals for assessing the performance of scramjet inlets with notched cowls

Mee, David J., Skowronski, Michael D. and Chiu, H. H. Sam (2002). Thermochromic liquid crystals for assessing the performance of scramjet inlets with notched cowls. Journal of the Indian Institute of Science Section B: Physical and Chemical Sciences, 82 (3&4), 145-160.

Boundary-layer transition measurements in hypervelocity flows in a shock tunnel

Mee, D. J. (2002). Boundary-layer transition measurements in hypervelocity flows in a shock tunnel. AIAA Journal, 40 (8), 1542-1548. doi: 10.2514/2.1851

Numerical investigations of flow and energy fields near a thermoacoustic couple

Ishikawa, Haruko and Mee, David J. (2002). Numerical investigations of flow and energy fields near a thermoacoustic couple. Journal of The Acoustical Society of America, 111 (2), 831-839. doi: 10.1121/1.1430687

Design, modelling and analysis of a six component force balance for hypervelocity wind tunnel testing

Smith, AL, Mee, DJ, Daniel, WJT and Shimoda, T (2001). Design, modelling and analysis of a six component force balance for hypervelocity wind tunnel testing. Computers & Structures, 79 (11), 1077-1088. doi: 10.1016/S0045-7949(01)00005-0

Measurement of the temperature field downstream of simulated leading-edge film-cooling holes

Mee, DJ, Ireland, PT and Bather, S (1999). Measurement of the temperature field downstream of simulated leading-edge film-cooling holes. Experiments in Fluids, 27 (3), 273-283. doi: 10.1007/s003480050352

Performance study of a power law starbody

Sabean, JW, Lewis, MJ, Mee, D and Paull, A (1999). Performance study of a power law starbody. Journal of Spacecraft and Rockets, 36 (5), 646-652. doi: 10.2514/2.3496

Developing a stress wave thrust balance for a hypersonic shock tunnel

Tuttle, S. L., Simmons, J. M. and Mee, D. J. (1997). Developing a stress wave thrust balance for a hypersonic shock tunnel. ICIASF Record, International Congress on Instrumentation in Aerospace Simulation Facilities, 1997, 362-367.

Turbulent spots in boundary layers in a free-piston shock-tunnel flow

Mee, D. J. and Goyne, C. P. (1996). Turbulent spots in boundary layers in a free-piston shock-tunnel flow. Shock Waves, 6 (6), 337-343. doi: 10.1007/BF02511324

Drag measurements in a hypervelocity expansion tube

Smith, AL and Mee, DJ (1996). Drag measurements in a hypervelocity expansion tube. Shock Waves, 6 (3), 161-166. doi: 10.1007/bf02510997

Three-component force balance for flows of millisecond duration

Mee, David J., Daniel, William J. T. and Simmons, John M. (1996). Three-component force balance for flows of millisecond duration. AIAA Journal, 34 (3), 590-595. doi: 10.2514/3.13108

Dynamic strain measurement using piezoelectric polymer film

Smith, AL and Mee, DJ (1996). Dynamic strain measurement using piezoelectric polymer film. Journal of Strain Analysis For Engineering Design, 31 (6), 463-465. doi: 10.1243/03093247V316463

Finite element modelling of a three-component force balance for hypersonic flows

Daniel W.J.T. and Mee D.J. (1995). Finite element modelling of a three-component force balance for hypersonic flows. Computers and Structures, 54 (1), 35-48. doi: 10.1016/0045-7949(94)00309-Q

Drag measurements at Mach 5 using a stress wave force balance

Tuttle S.L., Mee D.J. and Simmons J.M. (1995). Drag measurements at Mach 5 using a stress wave force balance. Experiments in Fluids, 19 (5), 336-341. doi: 10.1007/BF00203418

Experiments on supersonic combustion ramjet propulsion in a shock tunnel

Paull A., Stalker R.J. and Mee D.J. (1995). Experiments on supersonic combustion ramjet propulsion in a shock tunnel. Journal of Fluid Mechanics, 296 (-1), 159-183. doi: 10.1017/S0022112095002096

Scramjet thrust measurement in a shock tunnel

Paull A., Stalker R.J. and Mee D.J. (1995). Scramjet thrust measurement in a shock tunnel. Aeronautical Journal, 99 (984), 161-163. doi: 10.1017/s0001924000027147

Shock tunnel measurements of hypervelocity blunted cone drag

Porter L.M., Paull A., Mee D.J. and Simmons J.M. (1994). Shock tunnel measurements of hypervelocity blunted cone drag. AIAA journal, 32 (12), 2476-2477. doi: 10.2514/3.12318

UNCERTAINTY ANALYSIS IN TURBOMACHINE AND CASCADE TESTING

BAINES, NC, MEE, DJ and OLDFIELD, MLG (1991). UNCERTAINTY ANALYSIS IN TURBOMACHINE AND CASCADE TESTING. International Journal of Engineering Fluid Mechanics, 4 (4), 375-401.

LARGE CHORD TURBINE CASCADE TESTING AT ENGINE MACH AND REYNOLDS-NUMBERS

MEE, DJ (1991). LARGE CHORD TURBINE CASCADE TESTING AT ENGINE MACH AND REYNOLDS-NUMBERS. Experiments in Fluids, 12 (1-2), 119-124. doi: 10.1007/BF00226576

Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layer

Mee, D. J., Stalker, R. J. and Stollery, J. L. (1986). Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layer. Journal of Fluid Mechanics, 170 (9), 411-433. doi: 10.1017/S0022112086000952

Wall effects on sound propagation in tubes

Page N.W. and Mee D.J. (1984). Wall effects on sound propagation in tubes. Journal of Sound and Vibration, 93 (4), 473-480. doi: 10.1016/0022-460X(84)90416-4

Measurements of Free stream Density Fluctuations in the T4 Stalker Tube

Ananthapadmanaban, Ramprakash, Veeraragavan, Ananthanarayanan, McIntyre, Timothy, Wheatley, Vincent and Mee, David (2023). Measurements of Free stream Density Fluctuations in the T4 Stalker Tube. 25th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Karnataka, India, 28 May - 1 June 2023. Reston, VA United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-3031

Heat transfer measurements of the BOLT II flight experiment model within the T4 reflected shock tunnel

Landsberg, Will O., Sandral, Jacob, Mee, David and Veeraragavan, Anand (2023). Heat transfer measurements of the BOLT II flight experiment model within the T4 reflected shock tunnel. AIAA SCITECH 2023 Forum, National Harbor, MD USA/Online, 23-27 January 2023. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0087

Noise generated in a scramjet combustor

Ananthapadmanaban, Ramprakash, McIntyre, Tim, Wheatley, Vincent and Mee, David (2023). Noise generated in a scramjet combustor. AIAA SCITECH 2023 Forum, National Harbor, MD, United States, 23 - 27 January 2023. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2023-0314

Measurements of density fluctuations in a scramjet combustor

Ramprakash, A., McIntyre, T. J., Wheatley, V. and Mee, D. J. (2021). Measurements of density fluctuations in a scramjet combustor. Australian Combustion Symposium, Toowoomba, QLD Australia, 21-24 November 2021. Sydney, NSW Australia: Australia and New Zealand Combustion Institute.

A generalised calibration procedure for performing infrared thermography in expansion tubes

Ramesh, Ranjini, Morgan, Richard G. and Mee, David J. (2021). A generalised calibration procedure for performing infrared thermography in expansion tubes. AIAA Aviation Forum, Virtual, 2-6 August 2021. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2021-2981

Meanline Design and Off-Design Performance Prediction for Supercritical CO2 Radial Inflow Turbines

Lee, Sangkyoung, Mee, David, Guan, Zhiqiang and Gurgenci, Halg (2020). Meanline Design and Off-Design Performance Prediction for Supercritical CO2 Radial Inflow Turbines. 22nd Australasian Fluid Mechanics Conference AFMC2020, Brisbane, Australia, 7-10 December 2020. Brisbane, Australia: The University of Queensland. doi: 10.14264/6ce0260

Transition-Length Predictions for Hypersonic Flows with an Adverse Pressure Gradient

Convery-Brien, Isaac, Raghunath, Sreekanth and Mee, David (2020). Transition-Length Predictions for Hypersonic Flows with an Adverse Pressure Gradient. 22nd Australasian Fluid Mechanics Conference AFMC2020, Brisbane, Australia, 7-10 December 2020. Brisbane, QLD Australia: The University of Queensland. doi: 10.14264/929d0e1

Infrared thermography in expansion tubes for Martian entry flows

Ramesh, Ranjini, Morgan, Richard, Ravichandran, Ranjith and Mee, David (2020). Infrared thermography in expansion tubes for Martian entry flows. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Montréal, Québec, Canada, 10-12 March 2020. Reston, Virginia: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2020-2415

Static insertion loss, transmission loss and noise reduction testing of an acoustic louvre

Hayne, Michael, Tan, Dexter, Devereux, Richard and Mee, David J. (2020). Static insertion loss, transmission loss and noise reduction testing of an acoustic louvre. Acoustics 2019 - Sound Decisions: Moving forward with Acoustics, Cape Schanck, VIC, Australia, 10-13 November 2019. Australian Acoustical Society.

Magnetohydrodynamic drag force measurements in expansion tubes using an accelerometer

Smith, Daniel R., Gildfind, David E. , James, Christopher M., Andrianatos, Andreas, Mee, David J. and McIntyre, Timothy J. (2019). Magnetohydrodynamic drag force measurements in expansion tubes using an accelerometer. 32nd International Symposium on Shock Waves, Singapore, 14-19 July 2019. Singapore: Research Publishing Services. doi: 10.3850/978-981-11-2730-4_0145-cd

Removal of continuous extraneous noise from exceedance levels

Hugall, B., Brown, R. and Mee, D. J. (2019). Removal of continuous extraneous noise from exceedance levels. Australian Acoustical Society Annual Conference, AAS 2018, Adelaide, SA Australia, 7-9 November 2018. Toowong, QLD Australia: Australian Acoustical Society.

Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared Thermography

Ramesh, Ranjini, Kelly, Rory, Cullen, Timothy G., Morgan, Richard G. and Mee, David J. (2019). Shock Layer Radiation Measurements at a Mars Entry Condition for Infrared Thermography. AIAA Aviation 2019 Forum, Dallas, TX, United States, 17-21 June 2019. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2019-3006

Stress wave force balance sting design for magnetohydrodynamic drag force measurements in expansion tubes

Smith, Daniel R., Gildfind, David E., McIntyre, Timothy J. and Mee, David J. (2019). Stress wave force balance sting design for magnetohydrodynamic drag force measurements in expansion tubes. Asia Pacific International Symposium on Aerospace Technology (APISAT 2019), Gold Coast, QLD, Australia, 4-6 December 2019.

Testing and performance quantification of acoustic louvres

Hayne, Michael, Tan, Dexter, Devereux, Richard and Mee, David (2019). Testing and performance quantification of acoustic louvres. Australian Acoustical Society Annual Conference, AAS 2018, Adelaide, SA Australia, 7-9 November 2018. Toowong, QLD Australia: Australian Acoustical Society.

Dependence of turbulent Sspot initiation rates on hypersonic boundary layer flow parameters

Raghunath, Sreekanth , Narasimha, Roddam and Mee, David J. (2017). Dependence of turbulent Sspot initiation rates on hypersonic boundary layer flow parameters. 55th AIAA Aerospace Sciences Meeting and Exhibit, Dallas, TX, United States, 9-13 January 2017. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2017-1684

Boundary layer transition in hypersonic flows

Mee, D. J. and Raghunath, S. (2016). Boundary layer transition in hypersonic flows. Franco-Australian Symposium on Hypersonics and High Enthalpy Flows, Châtenay-Malabry, France, 7-9 September 2016.

Force Measurement in Impulse Hypersonic Facilities

Mee, D. J. (2016). Force Measurement in Impulse Hypersonic Facilities. First International Symposium on Hypersonics, Korean Advanced Institute of Science and Technology, 27-30 November 2016.

Performance Comparison of Distributed Injection Methods for Hypersonic Film-Cooling

Basore, K. D., Selzer, M., Wheatley, V., Boyce, R. R., Mee, D. J., Capra, B. R., Kuhn, M. and Brieschenk, S. (2016). Performance Comparison of Distributed Injection Methods for Hypersonic Film-Cooling. 20th Australasian Fluid Mechanics Conference, Perth, Western Australia, 5-8 December 2016. Victoria, Australia: Australasian Fluid Mechanics Society.

UQ research in transitional flows

Mee, D. J. and Raghunath, S. (2016). UQ research in transitional flows. 1st French-Australian Workshop on Re-entry and Hypersonic Aerothermodynamics, Brisbane, QLD, Australia, 23-25 February, 2016.

Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10

Doherty, Luke J., Smart, Michael K. and Mee, David J. (2015). Experimental testing of an airframe-integrated three-dimensional scramjet at Mach 10. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Atlanta, GA, United States, 16– 20 June 2014. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/1.J053785

Improving sound diffusion in a reverberation chamber

Mee, David J. and Vallis, Jack (2015). Improving sound diffusion in a reverberation chamber. Acoustics 2015, Hunter Valley, Australia, 15-18 November 2015. NSW Division of the Australian Acoustical Society.

Measurement of three-components of force on an airframe integrated scramjet at Mach 10

Doherty, Luke J., Smart, Michael K. and Mee, David J. (2015). Measurement of three-components of force on an airframe integrated scramjet at Mach 10. AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Glasgow, Scotland, 6-9 July 2015. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2015-3523

Turbulent spot initiation rates in boundary layers in a shock tunnel

Mee, D. J. and Tanguy, G. (2015). Turbulent spot initiation rates in boundary layers in a shock tunnel. International Symposium on Shock Waves, Madison, WI, United States, 14-19 July 2013. Cham, Switzerland: Springer. doi: 10.1007/978-3-319-16835-7_99

Experimental testing of an airframe integrated 3-D scramjet at true mach 10 flight conditions

Doherty, Luke J., Smart, Michael K. and Mee, David J. (2014). Experimental testing of an airframe integrated 3-D scramjet at true mach 10 flight conditions. AIAA AVIATION 2014 -19th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 2014, Atlanta, GA, United States, 16-20 June 2014. Reston, VA, United States: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/MHYTASP14

Ethylene augmentation of JP-8+100 in a supersonic combustor

Bateup, Mark L., Paull, Allan and Mee, David J. (2013). Ethylene augmentation of JP-8+100 in a supersonic combustor. JPC 2013: 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, United States, 14-17 July, 2013. Red Hook, NY, USA: Curran Associates. doi: 10.2514/6.2013-3700

Design of an airframe integrated 3-D scramjet and experimental results at a Mach 10 flight condition

Doherty, Luke J., Smart, Michael K. and Mee, David J. (2012). Design of an airframe integrated 3-D scramjet and experimental results at a Mach 10 flight condition. 18th AIAA/3AF International Space Planes and Hypersonics Systems and Technologies Conference, Tours, France, 24 - 28 September 2012. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-5910

Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustion

Wilson Chan, Mee, David J., Smart, Michael K. and Turner, James J. (2012). Effects of flow disturbances from cross-stream fuel injection on the drag reduction by boundary layer combustion. 18th AIAA/3AF International Space Planes and Hypersonic Systems and Technologies Conference, Tours, France, 24-28 September 2012. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2012-5889

Attitude guidance and control for a spinning, asymmetrical rocket payload

Creagh, Michael A. and Mee, David J. (2011). Attitude guidance and control for a spinning, asymmetrical rocket payload. AIAC14 Fourteenth Australian International Aerospace Congress, Melbourne, Australia, 28 February - 3 March 2011. Melbourne, Australia: Australian International Aerospace Congress.

Prediction of noise from small to medium sized crowds

Hayne, M. J., Taylor, J. C., Rumble, R. H. and Mee, D. J. (2011). Prediction of noise from small to medium sized crowds. Acoustics 2011: Breaking New Ground, Gold Coast, Australia, 2-4 November 2011. Darlinghurst, Australia: The Australian Acoustical Society.

Boundary layer combustion for viscous drag reduction in practical scramjet configurations

Chan, W. Y. K., Mee, D. J., Smart, M. K., Turner, J. C. and Stalker, R. J. (2010). Boundary layer combustion for viscous drag reduction in practical scramjet configurations. 27th International Congress of The Aeronautical Sciences (ICAS 2010), Nice, France, 19-24 September 2010. United Kingdom: Optimage.

Attitude guidance for spinning vehicles with independent pitch and yaw control

Michael Creagh and Mee, David J. (2009). Attitude guidance for spinning vehicles with independent pitch and yaw control. 47th AIAA Aerospace Sciences Meeting, Orlando , Florida, USA, 5-8 January 2009. Reston, VA, U.S.: American Institute of Aeronautics and Astronautics.

Force measurements and drag reduction

Mee, David J., Stalker, Raymond J., Suraweera, Milinda V., Tanimizu, Katsuyoshi, Kirchhartz, Rainer M., Ridings, Andrew N. and Chan, Wilson Y. K. (2008). Force measurements and drag reduction. Australian Hypersonics Capabilities and Future Directions Workshop 2008, Brisbane, Australia, 14-15 August 2008.

Skin Friction Drag with Boundary Layer Combustion in a Circular Combustor

Kirchhartz, Rainer M., Mee, David J. and Stalker, Raymond J. (2008). Skin Friction Drag with Boundary Layer Combustion in a Circular Combustor. 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, United States, 28 April - 1 May 2008. Reston, VA, United States: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2008-2589

Comparison of drag measurements of two axisymmetric scramjet models at Mach 6

Tanimizu, K., Mee, D. J. and Stalker, R. J. (2007). Comparison of drag measurements of two axisymmetric scramjet models at Mach 6. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 3-7 December, 2007. Brisbane, Australia: School of Engineering, The University of Queensland.

Effect of Boundary Layer Thickness and Entropy Layer on Boundary Layer Combustion

Kirchhartz, R. M., Mee, D. J. and Stalker, R. J. (2007). Effect of Boundary Layer Thickness and Entropy Layer on Boundary Layer Combustion. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 3-7 December, 2007. Brisbane, Australia: School of Engineering, The University of Queensland.

Numerical Simulation of a Ludwieg-tube Fuel Delivery System for Scramjet Experiments in Shock Tunnels

Gangurde, Dhananjay Y., Mee, David J. and Jacobs, Peter A. (2007). Numerical Simulation of a Ludwieg-tube Fuel Delivery System for Scramjet Experiments in Shock Tunnels. 16th Australasian Fluid Mechanics Conference (AFMC), Gold Coast, Queensland, Australia, 2-7 December 2007. Brisbane, Australia: School of Engineering, The University of Queensland.

Supersonic combustion experiments in the T4 Shock Tunnel

Mee, David J. (2007). Supersonic combustion experiments in the T4 Shock Tunnel. First International Conference on High Speed Transatmospheric Air and Space Transportation, Hyderabad, India, 29-30 June 2007. Aeronautical Society of India and the Astronautical Society of India.

Measurement and prediction of the force of an unfuelled axisymmetric scramjet model

Tanimizu, Katsuyoshi, Mee, David J. and Stalker, Raymond J. (2006). Measurement and prediction of the force of an unfuelled axisymmetric scramjet model. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2006-8064

Prediction of crowd noise

Hayne, M. J., Rumble, R. H. and Mee, D. J. (2006). Prediction of crowd noise. 1st Australasian Acoustical Societies' Conference 2006: Noise of Progress, ACOUSTICS 2006, , , November 20, 2006-November 22, 2006.

Scramjet flow visualization using Background Oriented Schlieren in hypersonic impulse facilities

Ramanah, Dwishen and Mee, David J. (2006). Scramjet flow visualization using Background Oriented Schlieren in hypersonic impulse facilities. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc.. doi: 10.2514/6.2006-8004

Measurement and prediction of the force of an unfuelled axisymmetric scramjet model

Tanimizu, K, Mee, D J and Stalker, R J (2006). Measurement and prediction of the force of an unfuelled axisymmetric scramjet model. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, 6-9 November 2006. USA: American Institute of Aeronautics and Astronautics.

Scramjet flow visualization using background oriented schlieren in hypersonic impulse facilities

Ramanah, D and Mee, D J (2006). Scramjet flow visualization using background oriented schlieren in hypersonic impulse facilities. 14th AIAA/AHI Space Plans and Hypersonic and Technologies Conference, Canberra, Australia, 6-9 November 2006. USA: American Institute of Aeronautics and Astronautics.

Influence of music genre and composition on entertainment noise limits

Hayne, Michael, Mee, David and Rumble, Ron (2005). Influence of music genre and composition on entertainment noise limits. Annual Conference of the Australian Acoustical Society 2005: Acoustics in a Changing Environment, Acoustics 2005, , , November 9, 2005-November 11, 2005.

Background oriented schlieren technique for flow visualisation in shock tunnels

Raghunath, S., Mee, D., Roesgen, T. and Jacobs, P. (2005). Background oriented schlieren technique for flow visualisation in shock tunnels. 25th International Symposium on Shock Waves- ISSW25, Bangalore, India, 17-22 July 2005. India: Universities Press.

Compressible, turbulent flow with boundary-layer heat addition

Denman, Andrew W., Jacobs, Peter A. and Mee, David J. (2005). Compressible, turbulent flow with boundary-layer heat addition. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 10 - 13 Jan 2005. Reston, Va.: American Institute of Aeronautics and Astronautics.

Flow establishment over rearward-facing steps in high enthalpy flows

Hayne, MJ, Mee, DJ, Gai, SL, Stewart, BS and Morgan, RG (2005). Flow establishment over rearward-facing steps in high enthalpy flows. 24th International Symposium on Shock Waves, Beijing Peoples R China, Jul 11-16, 2004. BERLIN: SPRINGER-VERLAG BERLIN. doi: 10.1007/978-3-540-27009-6_23

Influence of music genre and composition on entertainment noise limits

Hayne, Michael J., Mee, David J. and Rumble, Ron (2005). Influence of music genre and composition on entertainment noise limits. Acoustics 2005: Acoustics in a Changing Environment, Busselton, Western Australia, 9-11 November, 2005. Castlemaine, VIC, Australia: Australian Acoustical Society.

Real gas effects on flows over rearward-facing steps in high enthalpy flows

Hayne, M. J., Gai, S. L., Mee, D. J. and Morgan, R. G. (2005). Real gas effects on flows over rearward-facing steps in high enthalpy flows. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. doi: 10.1007/978-3-540-27009-6_36

Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer Combustion

Suraweera, Milinda, Mee, David J. and Stalker, Raymond J. (2005). Skin Friction Reduction in Hypersonic Turbulent Flow by Boundary Layer Combustion. 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 10-13 January, 2005. doi: 10.2514/6.2005-613

Flow establishment over rearward-facing steps in high enthalpy flows

Hayne, M. J., Mee, D. J., Gai, S. L., Stewart, B. S. and Morgan, R. G. (2004). Flow establishment over rearward-facing steps in high enthalpy flows. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer.

Flow visualization in the Drummond shock tunnel using the background oriented schlieren technique

Raghunath, S., Mee, D. J., Roesgen, T. and Jacobs, P. A. (2004). Flow visualization in the Drummond shock tunnel using the background oriented schlieren technique. 9th International Workshop on Shock Tube Technology, Woomera, South Australia, 27 September- 1 October 2004.

Performance measurements in a shock tunnel of a fuelled scramjet vehicle generating lift, thrust and pitching moment

Robinson, Matthew J. and Mee, David J. (2004). Performance measurements in a shock tunnel of a fuelled scramjet vehicle generating lift, thrust and pitching moment. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. doi: 10.1007/978-3-540-27009-6_134

Reducing skin friction by boundary layer combustion on a generic scramjet model

Trenker, M., Mee, D. J. and Stalker, R. J. (2004). Reducing skin friction by boundary layer combustion on a generic scramjet model. 24th International Symposium on Shock Waves, Beijing, China, 11-16 July 2004. Berlin, Germany: Springer. doi: 10.1007/978-3-540-27009-6_137

Simulation of the performance of a shock tube for studying chemical kinetics

Mee, D. J., Jacobs, P. A., Reddy, K. P. J., Rajakumar, B. and Arunan, E. (2004). Simulation of the performance of a shock tube for studying chemical kinetics. 9th International Workshop on Shock Tube Technology, Woomera, Australia, 27 September - 1 October 2004.

Three-component force measurements on a large scramjet in a shock tunnel

Robinson, M. J., Mee, D. J., Tsai, C. Y. and Bakos, R. J. (2004). Three-component force measurements on a large scramjet in a shock tunnel. USA: American Institute of Aeronautics and Astronautics, Inc. doi: 10.2514/1.10699

Visualization Of Supersonic Flows In Shock Tunnels, Using The Background Oriented Schlieren Technique

Raghunath, Sreekanth, Mee, David J., Roesgen, Thomas and Jacobs, Peter A. (2004). Visualization Of Supersonic Flows In Shock Tunnels, Using The Background Oriented Schlieren Technique. 2004 AIAA Australian Aerospace Student Conference, The University of Sydney, Sydney, 12 December, 2004.

Measurement of the aerodynamic performance of a scramjet-powered vehicle in a shock tunnel

Robinson, M. J., Mee, D. J. and Paull, A. (2003). Measurement of the aerodynamic performance of a scramjet-powered vehicle in a shock tunnel. Century of Aerospace Brisbane 2003, Brisbane, Queensland, Australia, 29 July - 1 August 2003. Barton, A.C.T., Australia: Engineers Australia.

Aeroassisted maneuvering of elastic tethered systems using a dissipative time-stepping algorithm

Jokic, M. D., Daniel, W. J. T., Asokanthan, S. F. and Mee, D. J. (2002). Aeroassisted maneuvering of elastic tethered systems using a dissipative time-stepping algorithm. 40th AIAA Aerospace Sciences Meeting, Reno, Nevada, USA, 14-17 January, 2002. USA: AIAA. doi: 10.2514/6.2002-1135

Drag on a slender cone at mach 6.6 with film ejection of hydrogen

Mee, D. J., Weiland, M.K.H. and Paull, A. (2002). Drag on a slender cone at mach 6.6 with film ejection of hydrogen. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23.

Heat transfer and flow behind a rearward facing step in a super-orbital expansion tube

Hayne, M. J., Gai, S.L., Hillier, R., Morgan, R. G., Mee, D. J. and Mcintyre, T. J. (2002). Heat transfer and flow behind a rearward facing step in a super-orbital expansion tube. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23.

Lift, pitching moment and thrust measurement on a fuelled scramjet

Robinson, M. J., Mee, D. J. and Paull, A. (2002). Lift, pitching moment and thrust measurement on a fuelled scramjet. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23.

Sonic jump for planetary entry vehicles

Abdel-Jawad, M., Morgan, R. G. and Mee, D. J. (2002). Sonic jump for planetary entry vehicles. 11th AIAA/AAAF International Conference Space Planes and Hypersonic Systems and Technologies, Orleans, France, 29/09/02-04/10/02. USA: American Institute of Aeronautics and Astronautics.

Sonic line location in reacting flows

Morgan, R. G., Abdel-Jawad, M. and Mee, D. J. (2002). Sonic line location in reacting flows. 40th AIAA Aerospace Sciences Meeting, Reno, Nevada, USA, 14-17 January, 2002. USA: AIAA. doi: 10.2514/6.2002-221

Stability tests in superorbital expansion tubes

Abdel-Jawad, M., Mee, D. J., Morgan, R. G. and Chiu, S.H. (2002). Stability tests in superorbital expansion tubes. 11th AIAA/AAAF International Conference Space Planes and Hypersonic Systems and Technologies, Orleans, France, 29/09/02 - 04/10/02. USA: American Institute of Aeronautics and Astronautics.

Transient force measurements at superorbital speeds

Abdel-Jawad, M., Mee, D. J., Morgan, R. G., Jacobs, P.A. and Philpot, J.A. (2002). Transient force measurements at superorbital speeds. Twenty-Third International Symposium on Shock Waves, The University of Texas at Arlington, USA, 23-27 July, 2001. USA: ISSW23.

Uncertainty analysis for the measurements of aerodynamic loss of cooled turbine blades

Aminossadati, S. M. and Mee, D. J. (2002). Uncertainty analysis for the measurements of aerodynamic loss of cooled turbine blades. The Fifth Biennial Engineering Mathematics and Applications Conference, Queensland University of Technology, Brisbane, 29/09/02 - 02/10/02. Brisbane, Australia: Queensland University of Technology.

A test facility for hypervelocity rarefied flows

Macrossan, Michael N., Chiu, H.- H. and Mee, David J. (2001). A test facility for hypervelocity rarefied flows. 22nd International Symposium on Rarefied Gas Dynamics (AIP Conference Proceedings), Sydney, Australia, 9-14 July, 2000. USA: American Institute of Physics. doi: 10.1063/1.1407637

Aerogravity assist manoeuvring of a tethered satellite system

Jokic, M. D., Asokanthan, S. F., Daniel, W. J. T. and Mee, D. J. (2001). Aerogravity assist manoeuvring of a tethered satellite system. AIAA Atmospheric Flight Mechanics Conference and Exhibit, Montreal, Canada, 6-9 August, 2001. USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2001-4071

Boundary layer transition measurements in hypervelocity flows in a shock tunnel

Mee, D. J. (2001). Boundary layer transition measurements in hypervelocity flows in a shock tunnel. 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 8-11 January, 2001. USA: American Institute of Aeronautics and Astronautics.

Heat transfer behind a step in high enthalpy super-orbital flow

Gai, S.L., Hayne, M. J., Gardner, A., Morgan, R. G. and Mee, D. J. (2001). Heat transfer behind a step in high enthalpy super-orbital flow. 39th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, USA, 8-11 January, 2001. USA: American Institute of Aeronautics and Astronautics. doi: 10.2514/6.2001-509

Heat transfer measurements in a transitional boundary layer on a flat plate in a hypervelocity flow

Mee, D. J. (2000). Heat transfer measurements in a transitional boundary layer on a flat plate in a hypervelocity flow. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, 18-20 September, 2000. Long Island, New York, USA: GASL.

Hyshot scramjet testing in the T4 shock tunnel

Frost, M., Paull, A., Alesi, H. and Mee, D. J. (2000). Hyshot scramjet testing in the T4 shock tunnel. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, 18-20 September, 2000. Long Island, New York, USA: GASL.

Simultaneous lift, moment and thrust measurement in hypervelocity flow

Robinson, M. J., Mee, D. J. and Paull, A. (2000). Simultaneous lift, moment and thrust measurement in hypervelocity flow. 7th International Workshop on Shock Tube Technology, Long Island, New York, USA, 18-20 September, 2000. Long Island, New York, USA: GASL.

Numerical investigations of thermoacoustic effects on isothermal plates

Ishikawa, H. and Mee, D. J. (1999). Numerical investigations of thermoacoustic effects on isothermal plates. 61st Meeting on Cryogenics and Superconductivity, Tokyo, 10-12 November 1999. Tokyo: Centre for Cryogenics and Superconductivity.

Performance study of a power law star body

Sabean, John W., Lewis, Mark J., Mee, David and Paull, Allan (1998). Performance study of a power law star body. 8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 1998, Norfolk, VA, April 27, 1998-April 30, 1998. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1998-1617

Pilot study for a rarefied hypervelocity test facility

Wendt M., Macrossan M., Jacobs P. and Mee D. (1998). Pilot study for a rarefied hypervelocity test facility. Proceedings of the 1998 Thirteenth Australasian Fluid Mechanics Conference, December 13, 1998-December 18, 1998. Monash University.

Mechanical and Space Engineering, a degree for undergraduates

Morgan R.G., Mee D.J. and Macrossan M.N. (1997). Mechanical and Space Engineering, a degree for undergraduates. 35th Aerospace Sciences Meeting and Exhibit, 1997, Reno, NV, United States, 6-9 January 1997. American Institute of Aeronautics and Astronautics Inc, AIAA.

Simulation of Aerodynamic Loss for Trailing-edge coolant ejection in gas turbine blades

Aminossadati, S.M. and Mee, D.J. (1995). Simulation of Aerodynamic Loss for Trailing-edge coolant ejection in gas turbine blades. 12th Australasian Fluid Mechanics Conference, Sydney , Australia, 10-15 December 1995. Sydney, N.S.W., Australia: University of Sydney.

Simulation of aerodynamic loss for trailing-edge coolant ejection in gas turbine blades

Aminossadat, S.M. and Mee, D.J. (1995). Simulation of aerodynamic loss for trailing-edge coolant ejection in gas turbine blades. The 12th Australasian Fluid Mechanics Conference, Sydney, NSW, Australia, 10-15 December 1995.

Lift, Drag and Thrust Measurement in a Hypersonic Impulse Facility

Tuttle, S. L., Mee, D. J. and Simmons, J. M. (1994). Lift, Drag and Thrust Measurement in a Hypersonic Impulse Facility. AIAA 18th Aerospace Ground Testing Conference, Colorado Springs, CO, 20-23 June, 1994. Reston, Virigina: American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1994-2596

Measurement of Scramjet Thrust in Shock Tunnels

Stalker, R. J., Simmons, J. M., Paull, A. and Mee, D. J. (1994). Measurement of Scramjet Thrust in Shock Tunnels. AIAA 18th Aerospace Ground Testing Conference, Colorado Springs, Colorado, USA, 20-23 June, 1994. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1994-2516

Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility

Paull, A., Stalker, R. J. and Mee, D. J. (1993). Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse Facility. AIAA and DGLR, 5th International Aerospace Planes and Hypersonics Technologies Conference, Munich, Germany, 30 November - 3 December, 1993. American Institute of Aeronautics and Astronautics Inc, AIAA. doi: 10.2514/6.1993-5168

3-COMPONENT AERODYNAMIC FORCE MEASUREMENTS IN HYPERVELOCITY IMPULSE FACILITIES

MEE, DJ, DANIEL, WJ and SIMMONS, JM (1992). 3-COMPONENT AERODYNAMIC FORCE MEASUREMENTS IN HYPERVELOCITY IMPULSE FACILITIES. 11th Australasian Fluid Mechanics Conference, Hobart Australia, Dec 14-18, 1992. HOBART: UNIVERSITY TASMANIA.

AN EXAMINATION OF THE CONTRIBUTIONS TO LOSS ON A TRANSONIC TURBINE BLADE IN CASCADE

MEE, DJ, BAINES, NC, OLDFIELD, MLG and DICKENS, TE (1992). AN EXAMINATION OF THE CONTRIBUTIONS TO LOSS ON A TRANSONIC TURBINE BLADE IN CASCADE. 35Th International Gas Turbine and Aeroengine Congress and Exposition, Brussels Belgium, Jun 11-14, 1990. NEW YORK: ASME-AMER SOC MECHANICAL ENG. doi: 10.1115/1.2927979

DETAILED BOUNDARY-LAYER MEASUREMENTS ON A TRANSONIC TURBINE CASCADE

MEE, DJ, BAINES, NC and OLDFIELD, MLG (1992). DETAILED BOUNDARY-LAYER MEASUREMENTS ON A TRANSONIC TURBINE CASCADE. 35Th International Gas Turbine and Aeroengine Congress and Exposition, Brussels Belgium, Jun 11-14, 1990. NEW YORK: ASME-AMER SOC MECHANICAL ENG. doi: 10.1115/1.2927980

Techniques for aerodynamic loss measurement of transonic turbine cascades with trailing-edge region coolant ejection

Mee, D. J. (1992). Techniques for aerodynamic loss measurement of transonic turbine cascades with trailing-edge region coolant ejection. American Society of Mechanical Engineers. doi: 10.1115/92GT157

A Comparison of Liquid Crystal Techniques for Transition Detection

Mee, D. J., Walton, T. W., Harrison, S. B. and Jones, T. V. (1991). A Comparison of Liquid Crystal Techniques for Transition Detection. AIAA 29th Aerospace Sciences Meeting, Reno, Nevada, 7-10 January, 1991.

An examination of the contributions to loss on a transonic turbine blade in cascade

Mee, D. J., Baines, N. C., Oldfield, M. L.G. and Dickens, T. E. (1990). An examination of the contributions to loss on a transonic turbine blade in cascade. ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition, GT 1990, Brussels, , June 11, 1990-June 14, 1990. American Society of Mechanical Engineers (ASME). doi: 10.1115/90-GT-264

Detailed boundary layer measurements on a transonic turbine cascade

Mee, D. J., Baines, N. C. and Oldfield, M. L.G. (1990). Detailed boundary layer measurements on a transonic turbine cascade. American Society of Mechanical Engineers (ASME). doi: 10.1115/90-GT-263

Investigation of Weak Shock-Shock and Shock-Expansion Intersection in the Presence of a Turbulent Boundary Layer

Mee, David J. and Stalker, R. J. (1987). Investigation of Weak Shock-Shock and Shock-Expansion Intersection in the Presence of a Turbulent Boundary Layer. AIAA 25th Aerospace Sciences Meeting, Reno, Nevada, 12-15 January, 1987.

Proceedings of the 16th Australasian Fluid Mechanics Conference

Peter Jacobs, Peter McIntyre, Matthew Cleary, David Buttsworth, David Mee, Rose, Clements, Richard Morgan and Charles Lemckert eds. (2007). Proceedings of the 16th Australasian Fluid Mechanics Conference. 16th Australasian Fluid Mechanics Conference, Gold Coast, QLD Australia, 3-7 December 2007. Brisbane, QLD Australia: The University of Queensland.

Acoustics 2004 - Transportation Noise and Vibration - the New Millennium

D. J. Mee, R. J. Hooker and I. D. M. Hillock eds. (2004). Acoustics 2004 - Transportation Noise and Vibration - the New Millennium. Proceedings of the annual conference of the Australian Acoustical Society, Gold Coast, Australia, 3-5 November 2004. Australia: Australian Acoustical Society.

Proceedings of the 10th Australian International Aerospace Congress

Mee, David J. ed. (2003). Proceedings of the 10th Australian International Aerospace Congress. 10th Australian International Aerospace Congress, Brisbane, Australia, 29 July – 1 August, 2003. Barton, Australia: Engineers Australia.

Operational manual for the X1 expansion tube

Chiu, S.H. and Mee, D. J. (2003). Operational manual for the X1 expansion tube. Research Report 2003/14 St. Lucia: Division of Mechanical Engineering, The University of Queensland.

Dynamic calibration of force balances

Mee, D. J. (2002). Dynamic calibration of force balances. Research Report 2002-6 Brisbane: Division of Mechanical Engineering, The Univ. of Qld.

Transition measurements on a 5 degree cone in the T4 Shock Tunnel

Mee, D. J. (2001). Transition measurements on a 5 degree cone in the T4 Shock Tunnel. Research Report 2001-2 St. Lucia: Mechanical Engineering Department, The University of Queensland.

Investigation of swept shock wave boundary layer interactions

Mee, David John (1987). Investigation of swept shock wave boundary layer interactions. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland.