David Mee
机构: The University of Queensland
每年引用次数
引用次数
引用: 2,633
H-指数: 29
I10-指数 : 65
出版物: 178
Measuring the Effect of Nose Bluntness on Drag of a Cone in a Hypervelocity Shock Tunnel Facility
L. M. Porter , A. Paull , D. J. Mee
Shock Waves @ Marseille I 53 -56
1995
Shock tunnel measurements of hypervelocity blunted cone drag
L. M. Porter , A. Paull , D. J. Mee , J. M. Simmons
AIAA Journal 32 ( 12) 2476 -2477
7
1994
Experiments on supersonic combustion ramjet propulsion in a shock tunnel
A. Paull , R. J. Stalker , D. J. Mee
Journal of Fluid Mechanics 296 ( -1) 159 -183
70
1995
An Examination of the Contributions to Loss on a Transonic Turbine Blade in Cascade
D. J. Mee , N. C. Baines , M. L. G. Oldfield , T. E. Dickens
Journal of Turbomachinery-transactions of The Asme 114 ( 1) 155 -162
53
1992
Detailed Boundary Layer Measurements on a Transonic Turbine Cascade
D. J. Mee , N. C. Baines , M. L. G. Oldfield
Journal of Turbomachinery-transactions of The Asme 114 ( 1) 163 -172
10
1992
Three-Component Force Measurements on a Large Scramjet in a Shock Tunnel
M. J. Robinson , D. J. Mee , C. Y. Tsai , R. J. Bakos
Journal of Spacecraft and Rockets 41 ( 3) 416 -425
20
2004
Dynamic calibration of force balances for impulse hypersonic facilities
D. J. Mee
Shock Waves 12 ( 6) 443 -455
105
2003
Background oriented schlieren for flow visualisation in hypersonic impulse facilities
D. Ramanah , S. Raghunath , D. J. Mee , T. Rösgen
Shock Waves 17 ( 1) 65 -70
23
2007
Large chord turbine cascade testing at engine Mach and Reynolds numbers
D. J. Mee
Experiments in Fluids 12 ( 1) 119 -124
7
1991
Techniques for aerodynamic loss measurement of transonic turbine cascades with trailing-edge region coolant ejection
D. J. Mee
ASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, GT 1992 1
33
1992
Drag measurements at Mach 5 using a stress wave force balance
S. L. Tuttle , D. J. Mee , J. M. Simmons
Experiments in Fluids 19 ( 5) 336 -341
34
1995
Performance measurements in a shock tunnel of a fuelled scramjet vehicle generating lift, thrust and pitching moment
M. J. Robinson , D. J. Mee
24th International Symposium on Shock Waves 1 885 -890
2005
Reducing skin friction by boundary layer combustion on a generic scramjet model
M. Trenker , D. J. Mee , R. J. Stalker
24th International Symposium on Shock Waves 1 903 -908
2005
Flow establishment over rearward-facing steps in high enthalpy flows
M. J. Hayne , D. J. Mee , S. L. Gai , B. S. Stewart
24th International Symposium on Shock Waves 1 173 -178
3
2005
Measurement of the temperature field downstream of simulated leading-edge film-cooling holes
D. J. Mee , P. T. Ireland , S. Bather
Experiments in Fluids 27 ( 3) 273 -283
10
1999
Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layer
D. J. Mee , R. J. Stalker , J. L. Stollery
Journal of Fluid Mechanics 170 ( -1) 411 -433
26
1986
Visualization Of Supersonic Flows In Shock Tunnels, Using The Background Oriented Schlieren Technique
David J. Mee , Sreekanth Raghunath , Peter A. Jacobs , Thomas Roesgen
Australian Aerospace Student Conference (AASC-2004)
3
2004
Proceedings of the 10th Australian International Aerospace Congress
David J. Mee
10th Australian International Aerospace Congress
2003
Supersonic combustion experiments in the T4 Shock Tunnel
David J. Mee
First International Conference on High Speed Transatmospheric Air and Space Transportation 288 -294
2007
Transition measurements on a 5 degree cone in the T4 Shock Tunnel
David J. Mee
Mechanical Engineering Department, The University of Queensland 1 -84
4
2001