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2001 Conference Publication Heat transfer behind a step in high enthalpy super-orbital flowGai, 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 |
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2000 Conference Publication Hyshot scramjet testing in the T4 shock tunnelFrost, 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. |
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2000 Conference Publication Heat transfer measurements in a transitional boundary layer on a flat plate in a hypervelocity flowMee, 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. |
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2000 Conference Publication Simultaneous lift, moment and thrust measurement in hypervelocity flowRobinson, 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. |
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1999 Journal Article Measurement of the temperature field downstream of simulated leading-edge film-cooling holesMee, 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 |
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1999 Conference Publication Numerical investigations of thermoacoustic effects on isothermal platesIshikawa, 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. |
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1999 Journal Article Performance study of a power law starbodySabean, 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 |
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1998 Conference Publication Performance study of a power law star bodySabean, 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 |
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1998 Conference Publication Pilot study for a rarefied hypervelocity test facilityWendt 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. |
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1997 Journal Article Developing a stress wave thrust balance for a hypersonic shock tunnelTuttle, 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. |
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1997 Conference Publication Mechanical and Space Engineering, a degree for undergraduatesMorgan 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. |
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1996 Journal Article Turbulent spots in boundary layers in a free-piston shock-tunnel flowMee, 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 |
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1996 Journal Article Drag measurements in a hypervelocity expansion tubeSmith, AL and Mee, DJ (1996). Drag measurements in a hypervelocity expansion tube. Shock Waves, 6 (3), 161-166. doi: 10.1007/bf02510997 |
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1996 Journal Article Three-component force balance for flows of millisecond durationMee, 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 |
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1996 Journal Article Dynamic strain measurement using piezoelectric polymer filmSmith, 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 |
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1995 Journal Article Finite element modelling of a three-component force balance for hypersonic flowsDaniel 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 |
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1995 Journal Article Experiments on supersonic combustion ramjet propulsion in a shock tunnelPaull 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 |
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1995 Conference Publication Simulation of Aerodynamic Loss for Trailing-edge coolant ejection in gas turbine bladesAminossadati, 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. |
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1995 Journal Article Scramjet thrust measurement in a shock tunnelPaull 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 |
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1995 Journal Article Drag measurements at Mach 5 using a stress wave force balanceTuttle 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 |
