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1995 Conference Publication Simulation of aerodynamic loss for trailing-edge coolant ejection in gas turbine bladesAminossadat, 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. |
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1994 Conference Publication Measurement of Scramjet Thrust in Shock TunnelsStalker, 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 |
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1994 Conference Publication Lift, Drag and Thrust Measurement in a Hypersonic Impulse FacilityTuttle, 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 |
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1994 Journal Article Shock tunnel measurements of hypervelocity blunted cone dragPorter 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 |
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1993 Conference Publication Thrust Measurements of a Complete Axisymmetric Scramjet in an Impulse FacilityPaull, 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 |
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1992 Conference Publication 3-COMPONENT AERODYNAMIC FORCE MEASUREMENTS IN HYPERVELOCITY IMPULSE FACILITIESMEE, 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. |
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1992 Conference Publication DETAILED BOUNDARY-LAYER MEASUREMENTS ON A TRANSONIC TURBINE CASCADEMEE, 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 |
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1992 Conference Publication Techniques for aerodynamic loss measurement of transonic turbine cascades with trailing-edge region coolant ejectionMee, 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 |
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1992 Conference Publication AN EXAMINATION OF THE CONTRIBUTIONS TO LOSS ON A TRANSONIC TURBINE BLADE IN CASCADEMEE, 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 |
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1991 Journal Article UNCERTAINTY ANALYSIS IN TURBOMACHINE AND CASCADE TESTINGBAINES, NC, MEE, DJ and OLDFIELD, MLG (1991). UNCERTAINTY ANALYSIS IN TURBOMACHINE AND CASCADE TESTING. International Journal of Engineering Fluid Mechanics, 4 (4), 375-401. |
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1991 Journal Article LARGE CHORD TURBINE CASCADE TESTING AT ENGINE MACH AND REYNOLDS-NUMBERSMEE, 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 |
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1991 Conference Publication A Comparison of Liquid Crystal Techniques for Transition DetectionMee, 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. |
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1990 Conference Publication An examination of the contributions to loss on a transonic turbine blade in cascadeMee, 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 |
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1990 Conference Publication Detailed boundary layer measurements on a transonic turbine cascadeMee, 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 |
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1987 Other Outputs Investigation of swept shock wave boundary layer interactionsMee, David John (1987). Investigation of swept shock wave boundary layer interactions. PhD Thesis, School of Mechanical and Mining Engineering, The University of Queensland. doi: 10.14264/284113 |
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1987 Conference Publication Investigation of Weak Shock-Shock and Shock-Expansion Intersection in the Presence of a Turbulent Boundary LayerMee, 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. |
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1986 Journal Article Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layerMee, 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 |
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1984 Journal Article Wall effects on sound propagation in tubesPage 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 |
