CFD analysis of the CIAM/NASA scramjet

38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2002, Pages

  Rodriguez, C G ^a  

^a Allied Aerospace   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUAL OPERATION; CHEMISTRY MODELS; DESIGN AND CONSTRUCTION; DUAL-MODE OPERATION; GRID CONVERGENCE; HIGH-SPEED CONDITIONS; HYSTERESIS EFFECT; TURBULENT SCHMIDT NUMBER;

PROPULSION;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84896848968     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (11)

1. McClinton, C., Roudakov, A., Semenov, V., and Kopehenov, V., "Comparative Flow Path Analysis and Design Assessment of an Axisymmetric Hydrogen Fueled Scramjet Flight Test Engine at a Mach Number of 6.5", AIAA Paper 96-4571, 1996.
2. Voland, R.T., Auslender, A.H., Smart, M.K., Roudakov, A., Semenov, V., and Kopehenov, V., "CIAM/NASA Mach 6.5 Scramjet Flight and Ground Test", AIAA 99-4848, 1999.
3. Hawkins, R.W., "CFD Analysis of Oversped CIAM Scramjet at Mach 6.5", HNAG Report 96-1-071, NASA Langley Research Center, 1996.
4. Gaffney, R.L., and Sanetrik, M.D., "CFD Calculation of the CIAM SCRAMJET Engine Flowfield", unpublished report, 1999.
5. Rodriguez, C.G. "CFD Analysis of the CIAM/NASA Scramjet Engine (I): Inlet and Scramjet Analysis", HX Report HX-977, NASA Langley Research Center, 2001.
6. Rodriguez, C.G. "CFD Analysis of the CIAM/NASA Scramjet Engine (II): Inlet Unstart and Restart", HX Report HX-977, NASA Langley Research Center, 2001.
7. White, J.A., and Morrison, J.H., "A Pseudo-Temporal Multi-Grid Relaxation Scheme for Solving the Parabolized Navier-Stokes Equations", AIAA 99-3360, 1999.
8. Wilcox, D.C., Turbulence Modeling for CFD, 2nd. Edition, DCW Industries, Inc., 1998.
9. Drummond, J.P., Rogers, R.C., and Hussaini, M.Y., "A Detailed Numerical Model of a Supersonic Reacting Mixing Layer", AIAA 86-1427, 1986.
10. Rogers, R.C., "A Study of the Mixing of Hydrogen Injected Normal to a Supersonic Airstream", NASA TN D-6114, 1971.
11. Eklund, D.R., Baurle, R.A., and Gruber, M.R., "Numerical Study of a Scramjet Combustor Fueled by an Aerodynamic Ramp Injector in Dual-Mode Combustion", AIAA Paper 2001-0379, 2001.