Compressible, turbulent flow with boundary-layer heat addition

Andrew Denman , Peter Jacobs , David Mee
43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers 1 -10

8
2005
Skin Friction Drag with Boundary Layer Combustion in a Circular Combustor

Rainer Kirchhartz , David Mee , Raymond Stalker
15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference 1 -10

8
2008
Infrared Thermography in Expansion Tubes for Martian Entry Flows

Ranjini Ramesh , Richard Morgan , Ranjith Ravichandran , David Mee
23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2020

1
2020
Heat Transfer Measurements of the BOLT II Flight Experiment Model within the T4 Reflected Shock Tunnel

Will O Landsberg , Jacob Sandral , David Mee , Anand Veeraragavan
0087 -0087

2023
This is the author-manuscript version of this work-accessed from

JT Madhani , D Pendrey , Rong Situ , Richard J Brown
Assessment 2 7 -7

2007
Measurements of Free stream Density Fluctuations in the T4 Stalker Tube

Ramprakash Ananthapadmanaban , Ananthanarayanan Veeraragavan , Timothy McIntyre , Vincent Wheatley
3031 -3031

2023
Background oriented schlieren technique for flow visualisation in shock tunnels

S Raghunath , David Mee , Thomas Rösgen , Peter Jacobs
Shock Waves: Proceedings of the 25th International Symposium on Shock Waves 14 ( 5-6) 425 -426

2005
5
2014
Improving sound diffusion in a reverberation chamber

Jack Vallis , Michael Hayne , David Mee , Richard Devereux
Proceedings of the Acoustics

8
2015
Testing and performance quantification of acoustic louvres

Michael Hayne , Dexter Tan , Richard Devereux , David Mee
Proceedings of ACOUSTICS 7 -9

2
2018
A Calibration Procedure for Performing Infrared Thermography in Expansion Tubes

Ranjini Ramesh , Richard Morgan , David Mee
2981 -2981

1
2021
Self Ignition of Hydrogen-Air Mixtures with Inclined Porthole Injection in Supersonic Flows

Rainer Kirchhartz , Allan Paull , David Mee , Herbert Olivier
International Journal of Hypersonics

2012
This is the author-manuscript version of this work-accessed from http://eprints. qut. edu. au

David Butsworth , David Mee , Rose Clements , Richard Morgan

2007
Heat transfer and flow behind a step in high enthalpy superorbital flow

SL Gai , DJ Mee , RG Morgan , TJ McIntyre
Aeronautical Journal 107 ( 1073) 435 -442

9
2003
Comparison of force measurements in the HEG and T4 shock tunnels

DJ Mee , A Paull , Mkh Weiland , WH Beck
Proceedings of the Third European Symposium On Aerothermodynamics for Space Vehicles 420 631 -635

2
1999
New Techniques for Force and Pressure Measurement in Hypervelocity Impulse Facilities

DJ Mee , JM Simmons , SL Tuttle , WJ Daniel
International Aerospace Congress 1995: Proceedings; Second Pacific International Conference on Aerospace and Technology; Sixth Australian Aeronautical Conference 935

1995
Hybrid Rocket Design Concepts and Techniques

S Oberhollenzer , M D'Souza , TT He , DJ Mee
5th NSSA Australian Space Science Conference: 14 to 16 September 2005 Hosted by RMIT University, Melbourne, Australia 176

2005
An examination of the contributions to loss on a transonic turbine blade in cascade

DJ Mee , NC Baines , MLG Oldfield , TE Dickens
Turbo Expo: Power for Land, Sea, and Air 79085 V005T16A012 -V005T16A012

29
1990
Detailed boundary layer measurements on a transonic turbine cascade

DJ Mee , NC Baines , MLG Oldfield
Turbo Expo: Power for Land, Sea, and Air 79047 V001T01A092 -V001T01A092

3
1990
AERONAUTICAL

FS Lien , MA Leschziner , G Bouwer , AL Gaitonde

1