Skip to menu Skip to content Skip to footer

2002

Conference Publication

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.

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

2002

Conference Publication

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 jump for planetary entry vehicles

2002

Other Outputs

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.

Dynamic calibration of force balances

2002

Conference Publication

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

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

2002

Conference Publication

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.

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

2001

Journal Article

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

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

2001

Conference Publication

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 behind a step in high enthalpy super-orbital flow

2001

Other Outputs

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.

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

2001

Conference Publication

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.

Boundary layer transition measurements in hypervelocity flows in a shock tunnel

2001

Conference Publication

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

Aerogravity assist manoeuvring of a tethered satellite system

2001

Conference Publication

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

A test facility for hypervelocity rarefied flows

2000

Conference Publication

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.

Hyshot scramjet testing in the T4 shock tunnel

2000

Conference Publication

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.

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

2000

Conference Publication

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.

Simultaneous lift, moment and thrust measurement in hypervelocity flow

1999

Journal Article

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

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

1999

Conference Publication

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.

Numerical investigations of thermoacoustic effects on isothermal plates

1999

Journal Article

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

Performance study of a power law starbody

1998

Conference Publication

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.

Pilot study for a rarefied hypervelocity test facility

1998

Conference Publication

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

Performance study of a power law star body

1997

Journal Article

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.

Developing a stress wave thrust balance for a hypersonic shock tunnel