Numerical study of jet injection into a supersonic crossflow

35th Joint Propulsion Conference and Exhibit

Volumn , Issue , 1999, Pages

  Tam, Chung Jen ^a   Baurle, Robert A ^a   Gruber, Mark R ^b  

^a WRIGHT PATTERSON AIR FORCE BASE   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL FLUID DYNAMICS; FLUID DYNAMICS; FUELS; NOZZLES; PROPULSION; SUPERSONIC AERODYNAMICS; TURBULENCE MODELS;

COMPUTATIONAL DOMAINS; DYNAMIC MECHANISM; INFLOW CONDITIONS; INJECTION NOZZLES; NUMERICAL RESULTS; PLUME PENETRATION; SURFACE PRESSURES; TWO-EQUATION TURBULENCE MODELS;

FIGHTER AIRCRAFT;

EID: 84963853524     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)

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2. Heister, S.D. and Karagozian, A.R., “Gaseous Jet in Supersonic Crossflow,” AIAA Journal, Vol. 28, No. 5, May 1990, pp. 819-827.
3. Kamotani, Y. and Greber, I., “Experiments on a Turbulent Jet in Crossflow,” AIAA Journal, Vol. 10, Nov. 1972, pp. 1425-1429.
4. Fearn, R. and Weston, R.P., “Vorticity Associated with a Jet in Cross Flow,” AIAA Journal, Vol. 12, Dec. 1974, pp. 1666-1671.
5. McDaniel, J.C. and Graves, J., “Laser-Induced Fluorescence Visualization of Transverse Gaseous Injection in a Nonreacting Supersonic Combustor,” Journal of Propulsion and Power, Vol. 4, Nov-Dec. 1988, pp. 591-597.
6. White, J. A. and Morrison, J. H., “A Pseudo-Temporal Multi-Grid Relaxation Scheme for Solving the Parabolized Navier-Stokes Equations,” AIAA Paper 99-3360, June 1999.
7. Gruber, M.R., Nejad, A.S., Chen, T.H. and Dutton, J.C., “Compressibility Effects in Supersonic Transverse Injector Flowfield,” Physics of Fluids, Vol. 9, No.5,1997, pp. 1448-1461.
8. Gruber, M.R., Nejad, A.S., Chen, T.H. and Dutton, J.C., “Bow Shock/Jet Interaction in Compressible Transverse Injection Flowfields,” AIAA Journal, Vol. 34, No. 10,1996, pp. 2191-2193.
9. Gruber, M.R., Nejad, A.S., Chen, T.H. and Dutton, J.C., “Large Structure Convection Velocity, Measurements in Compressible Transverse Injection Flowfields.” Experiments in Fluids, Vol. 22, 1997, pp. 397-407.
10. Menter, F.R., “Zonal Two Equation k-w Models for Aerodynamic Flows,” AIAA Paper 93-2906, July 1993.
11. Wilcox, D.C., “Turbulence Modeling for CFD, 2nd Edition,” DCW Industries, Inc., 1998.
12. Wilcox, D.C., “Reassessment of the Scale-Determining Equation for Advanced Turbulence Models,” AIAA Journal, Vol. 26, Nov. 1988, pp. 1299-1310.
13. Jones, W.P. and Launder, B.E., “The Prediction of Laminarization with a Two Equation Model of Turbulence,” International Journal of Heat and Mass Transfer, Vol. 15,1972, pp. 310-314.
14. Baurle, R.A., Mathur, T., Gruber, M.R., and Jackson, K.R., “A Numerical and Experimental Investigation of a Scramjet Combustor for Hypersonic Missile Applications,” AIAA Paper 98-3121, July 1998.