Evaluation of pressure oscillations by a laboratory motor

Author:

TAHERINEZHAD Roohollah,ZAREPOUR Gholamreza

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference62 articles.

1. Determination of triggering condition of vortex-driven acoustic combustion instability in rocket motors;Wu;J Propul Power,2000

2. Shape effects of single axisymmetric cavity in a circular duct on flow induced acoustic oscillations;Thirumoorthy;Aerosp Sci Technol,2017

3. Vortex-sound generated pressure oscillations simulation in internal flow by means of Q-1D model;Ferretti,2011

4. Numerical simulation of aeroacoustic phenomena in a solid rocket booster;Cosyn;J Spacecraft Rockets,2005

5. A subscale test program to assess the vortex shedding driven instabilities in segmented solid rocket motors;Traineau,1997

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