Two-dimensional numerical simulation of the stability of a solid propellant rocket motor-Reference-Cited by-同舟云学术

Two-dimensional numerical simulation of the stability of a solid propellant rocket motor

Published:1991-01-07 Issue: Volume: Page:
ISSN:
Container-title:29th Aerospace Sciences Meeting
language:
Short-container-title:

Author:

LUPOGLAZOFF NICOLAS¹,VUILLOT FRANCOIS¹

Affiliation:

1. ONERA, Chatillon, France

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1991-205

Reference9 articles.

1. [l] SABNISJ.,GIBELINGH.J. MCDONALD H. "Calculation of solid r o e l l a nt rocket motor internal flow field using'anLimplicitNavier-Stokes procedure". AIAA Paper 85-1625. AIAA 18th Fluid Dynamics, Plasma Dynamics and Laser Conference,July 1985. HSIEH K.C., YANG V., TSENG I.S. "Navier-Stokes calculation of solid propellant rocket motor internal flow fields". AIAA Paper 68-3182. AIAA 24th Joint Pro ulsion Conference, Boston (Massachusett)U A.~ u l 1988. CHANG I.S. "Three-dimensional, two phase, transonic, canted nozzle flows". AIAA Paper 88-3201. AIAA 24th Joint Propulsion Conference, Boston (Massachusett)USA,July 1988. MAJUMDAR A.K., WHITESIDES R., JENKINS S.L.BACCHUSD.L. "Circonferential flow analysis atthe aft fieldjoint of the space shuttle solid rocket motor". AIAA Paper 88-3319. AIAA 24th Joint Propulsion Conference, Boston (Massachusett) USA,July 1988.

2. AVALON G. and VUILLOT F. "Prevision du comportement instationnaire d'une tuyere amorcee". 25Pme Colloque d'Aerodynamique Appliquee (AAAF), Talence, 12-14 octobre 1988. ONERATP 1988-149.

3. Nonreflecting boundary conditions for nonlinear hyperbolic systems

4. A numerical model of acoustic choking, Part I: Shock free solutions

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