Comparison of supersonic combustion tests with shock tunnels, flight and CFD

Collection of Technical Papers - AIAA/ASME/SAE/ASEE 42nd Joint Propulsion Conference

Volumn 5, Issue , 2006, Pages 3629-3642

  Steelant, J ^a,c   Mack, A ^a,c   Hannemann, K ^b   Gardner, A D ^b  

^a EUROPEAN SPACE AGENCY   (Netherlands)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

^c Division of Propulsion and Aerothermodynamics   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

EQUIVALENCE RATIO; HIGH ENTHALPY SHOCK TUNNEL (HEG); SHOCK TUNNELS; SUPERSONIC COMBUSTION;

COMBUSTION; COMPUTATIONAL FLUID DYNAMICS; ENTHALPY; NUMERICAL METHODS; SHOCK TUBES; TOPOLOGY;

SUPERSONIC AERODYNAMICS;

EID: 34249293033     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Paull, A.,Scramjet measurements in a shock tunnel. AIAA 99-2450, 1999
2. Beck, W.H., Hannemann, K., Weiland, M., Modifications to the DLR high enthalpy shock tunnel HEG for measurements on supersonic combustion. AIAA 2001-1860, 2001
3. Paull, A., Alesi, H., Anderson, S., HyShot flight program and how it was developed, AIAA 2002-4939, 2002
4. Gardner, A.D., Hannemann, K., Evaluation of Full Engine Scramjet technology. DLR-IB 224-2004 A 11, 2004
5. Gardner, A.D., Hannemann, K., Steelant, J., Paull, A. Ground Testing of the HyShot Supersonic Combustion Flight Experiment in HEG and Comparison with Flight Data, AIAA 2004-3345, 2004
6. Mack, A., Hannemann, V., Validation of the Unstructured DLR-TAU-Code for Hypersonic Flows, AIAA 2002-3111
7. th STAB Symposium, Bremen, Germany, November 16-18, 2004
8. Kovar, A., Schülein, E., Comparison of Experimental and Numerical Investigations on the Side Jets in a supersonic Cross Flow. Royal Aeronautical Society, London, Great Britain, September 14-15, 2004
9. Karl, S., Hannemann, K., Application of the DLR Tau-code to the RCM-1 testcase: Penn State Preburner Combustor. Proceedings of the 3rd International Workshop on Rocket Combustion Modeling, 2006
10. Evans, J.S., Schexnayder Jr., C.J., Influence of Chemical Kinetics and Unmixedness on Burning in Supersonic Hydrogen Flames AIAA Journal, Vol. 18, No. 2, February 1980