DES validations of cavity acoustics over the subsonic to supersonic range

Collection of Technical Papers - 10th AIAA/CEAS Aeroacoustics Conference

Volumn 1, Issue , 2004, Pages 731-741

  Allen, Richard ^a,b   Mendonça, Fred ^a,c  

^a SIEMENS AG   (Germany)

^b Engineering Services Department   (United Kingdom)

^c CFD Engineering Services   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BROADBAND SPECTRA; CAVITY ACOUSTICS; DETACHED EDDY SIMULATION (DES); MACH NUMBER;

COMPUTATIONAL FLUID DYNAMICS; COMPUTER SIMULATION; DATA REDUCTION; FREQUENCIES; SUPERSONIC AERODYNAMICS; TURBULENCE;

SUBSONIC AERODYNAMICS;

EID: 19644381897     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Henshaw M.J de C., "M219 Cavity case in Verification and Validation Data for Computational Unsteady Aerodynamics", RTO-TR-26, AC/323(AVT)TP/19, October 2000.
2. th AIAA/CEAS Aeroacoustics Conference, May 2003.
3. Ross J.A., QinetiQ, Bedford, MK41 6AE, UK
4. STAR-CD Version 3.20 User Guide and Methodology Manuals, CD adapco Group, London, UK, 2004.
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", First AFOSR International Conference on DNA/LES, Ruston, Louisiana, USA, 1997.
6. Travin, A., Shur, M., Strelets, M., Spalart, P., "Physical and Numerical Upgrades in the Detached-Eddy Simulation of Complex Turbulent Flows", Advances in LES of Complex Flows, edited by P Friedrich and W.Rodi, Kluwer Academic Publishers, 2002, pp. 239-254.
7. Issa, R.I., Gosman, A.D., and Watkins, A.P., The computation of compressible and incompressible recirculating flows by a non-iterative implicit scheme, J. Comp. Phys., No. 62, 1986, pp. 66-82.
8. Allen, R. and Mendonça, F., "DES Predictions on the M219 Cavity at M=0.85", Colloquium EUROMECH 449, Chamonix, France, December 9-12, 2003