The HyShot scramjet flight experiment - flight data and CFD calculations compared

12th AIAA International Space Planes and Hypersonic Systems and Technologies

Volumn , Issue , 2003, Pages

  Boyce, Russell R ^a   Gerard, Sullivan ^a   Paull, Allan ^b  

^a UNIVERSITY OF NEW SOUTH WALES   (Australia)

^b UNIVERSITY OF QUEENSLAND   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; BOUNDARY LAYERS; COMBUSTION; RAMJET ENGINES;

ANGLES OF ATTACK; FLIGHT DATA; FLIGHT EXPERIMENTS; HIGH ANGLES OF ATTACK; LOCAL MINIMUMS; SUPERSONIC COMBUSTION;

SUPERSONIC AIRCRAFT;

EID: 85065094091     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-7029     Document Type: Conference Paper

References (6)

1. Aerosoft Inc. GASPex Version 3. The General Aerodynamic Simulation Program -Computational Flow Analysis Software for the Scientist and Engineer, User's Manual, Aerosoft, Inc., VA., 1997.
2. nd International Symposium on Shock Waves, London, 1999.
3. Boyce, RR, Paull, A,"Scramjet Intake and Exhaust CFD Studies for the HyShot Scramjet Flight Experiment", AIAA-2001-1891, 2001.
4. Boyce, RR, Frost, M, Paull, A "Combustor and Nozzle CFD Calculations for the HyShot Scramjet Flight Experiment", CFD Journal, Vol. 12, No. 2-3, 2003 (to be published).
5. Paull, A "The HyShot flight program and how it was developed", AIAA-2002-5248, 2002.
6. Evans, JS, Schexnayder, CJ "Influence of Chemical Kinetics and Unmixedness on Burning in Supersonic Hydrogen Flows", AIAA J., v. 18, no. 2, pp. 188-193, 1979.