Simulation of a sonic jet injected into a supersonic cross-flow

Proceedings of the 16th Australasian Fluid Mechanics Conference, 16AFMC

Volumn , Issue , 2007, Pages 608-612

  Higgins, K ^a   Schmidt, S ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

AIR CROSS-FLOW; AIR JET; BARREL SHOCK; BOW SHOCK WAVE; COUNTER-ROTATING VORTEX PAIR; CROSS FLOWS; EXPERIMENTAL MEASUREMENTS; EXPERIMENTAL STUDIES; GRID RESOLUTION; HYBRID RANS-LES; JET PLUMES; MACH DISK; PEAK VALUES; RECIRCULATION REGIONS; REYNOLDS STRESS; SHEAR LAYER; SONIC JETS; TURBULENT KINETIC ENERGY; VELOCITY FLUCTUATIONS; VORTICAL STRUCTURES;

FLUID MECHANICS; REYNOLDS NUMBER; VORTEX FLOW;

SUPERSONIC AERODYNAMICS;

EID: 77955535411     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Baurle, R. A., Tam, C. J., Edwards, J. R. and Hanson, H. A., Hybrid simulation approach for cavity flows: blending, algorithm and boundary treatment issues, AIAA Journal, 41, 2003, 1463-1480.
2. Ben-Yakar, A., Mungal, M. G. and Hanson, R. K., Time evolution and mixing characteristics of hydrogen and ethylene transverse jets in supersonic crossflows, Phys. Fluids, 18, 2006, 026101.
3. Peterson, D. M., Subbareddy, P. K. and Candler, G. V., Assessment of synthetic inflow generation for simulating injection into a supersonic crossflow, AIAA 2006-8128.
4. Santiago, J. C., An experimental study of the velocity field of a transverse jet injected into a supersonic crossflow, Ph.D. thesis, University of Illinois, Urbana-Champaign, 1995.
5. Spalart, P. R., Jou, W. H., Strelets, M. and Allmaras, S. R., Comments on the feasibility of LES for wings, and on a hybrid RANS/LES approach, in Advances in DNS/LES, editors C. Liu and Z. Liu, Greyden, Columbus, 1997.
6. Strelets, M., Detached eddy simulation of massively separated flows, AIAA 2001-0879.
7. VanLerberghe, W. M., Santiago, J. G., Dutton, J. C. and Lucht, R. P., Mixing of a sonic transverse jet injected into a supersonic flow, AIAA Journal, 38, 2000, 470-479. (Pubitemid 30560910)
8. White, J. A. and Morrison, J. H., A pseudo-temporal multigrid relaxation scheme for solving the parabolized Navier-Stokes equations, AIAA 99-3360.