Prediction of longitudinal combustion instabilities in axisymmetrical propellant grains

Author:

PHILIPPE A.1,TCHEPIDJIAN P.1

Affiliation:

1. SocieteNationale des Poudres et Explosifs, Centre de Recherches du Bouchet, Vert-le-Petit, Essonne, France

Publisher

American Institute of Aeronautics and Astronautics

Reference6 articles.

1. C.P.1.A Publication n' 191, (15651 - 2 F.E.C. CULICK

2. burner testing of metallized solirl propellants". AFWL - TR 74-28, (1974). 3 F.E.C. CUISCK

3. "A review of calculations for Unsteady burnirq of solid propellants". A.I.A.A.Journal,no12, &A, (1'160). 4 F.E.C. CULICK

4. "umericalanalysis of nonlinear longitudinal combustion instability In metallized propellant solid rocket motors. AFWL - TR 72-88, (1972). h - P. KUENTZMANN

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Experimental evaluation of one-dimensional design technology for linear combustion instability;30th Joint Propulsion Conference and Exhibit;1994-06-27

2. Solid Propellant Combustion and Internal Ballistics of Motors;Solid Rocket Propulsion Technology;1993

3. Solid Propellant Grain Design;Solid Rocket Propulsion Technology;1993

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