Qualitative model of vortex induced oscillations in a model of solid propellant boosters

4th AIAA/CEAS Aeroacoustics Conference

Volumn , Issue , 1998, Pages

  Anthoine, J ^a   Olivari, D ^a   Hulshoff, S ^b   Van Rooij, M ^b  

^a VON KARMAN INSTITUTE FOR FLUID DYNAMICS   (Belgium)

^b EINDHOVEN UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AEROACOUSTICS; NOZZLE DESIGN; POROUS PLATES; PROPELLANTS; ROCKET ENGINES;

EULER COMPUTATIONS; FLOW-ACOUSTIC COUPLING; QUALITATIVE MODEL; SOLID ROCKET MOTORS; SOLID-PROPELLANT BOOSTERS; SOUND PRODUCTION; VORTEX-INDUCED OSCILLATIONS; VORTICAL STRUCTURES;

SOLID PROPELLANTS;

EID: 84977103219     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1998-2270     Document Type: Conference Paper

References (8)

1. Dotson, K.W. ; Koshigoe, S. and Pace, K.K.: "Vortex shedding in a Large Solid Rocket Motor Without Inhibitors at the Segment Interfaces", J. of Propulsion and Power, Vol. 13, No. 2, March-April 1997, pp. 197-206.
2. Brown, R.S. and al.: "Vortex shedding as an additional source of acoustic energy in segmented solid propellant rocket motors", AIAA/SAE/ASME 16th Conference, Hartford, U.S.A., 1980.
3. Plateau, A. ; Van Moorhem, W.: "Prediction of vortex shedding responses in segmented solid rocket motors", AIAA Paper 90-2073.
4. th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, January 12-15, 1998, Paper AIAA-98-0475.
5. Bird, R.B. ; Stewart, W.E. ; Lightfoot, E.N.: "Transport Phenomena", John Wiley & Sons Inc., 1960.
6. Thompson, K. W.: "Time-Dependent Boundary Conditions for Hyperbolic Systems", Journal of Computational Physics, 68 1-24 (1987) and 89, 439-461 (1990)
7. Poinsot, T. J. and Lele, S. K.: "Boundary Conditions for the Direct Simulation of Compressible Viscous Flows", Journal of Computational Physics, 101, 104-129, (1992)
8. ème Colloque R&D "Ecoulements Internes en Combustion Solid" ONERA/CNES/ENSMA, Poitiers, France, 25-27 March, 1998.