Prediction and Analysis of Combustion Instabilities in a Model Rocket Engine-Reference-Cited by-同舟云学术

Prediction and Analysis of Combustion Instabilities in a Model Rocket Engine

Published:2014-07 Issue:4 Volume:30 Page:978-990
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Selle Laurent¹,Blouquin Rodolphe²,Théron Marie³,Dorey Luc-Henry⁴,Schmid Martin⁵,Anderson William⁶

Affiliation:

1. Centre National de la Recherche Scientifique, Institut de Mécanique des Fluides de Toulouse, F-31400 Toulouse, France

2. Bertin Technologies, F-78180 Montigny-le-Bretonneux, France

3. Centre National d’Etudes Spatiales, F-75612 Paris, France

4. ONERA, F-92322 Châtillon, France

5. Technische Universität München, D-85748 Garching, Germany

6. School of Aeronautics and Astronautics, Purdue University, West Lafayette, Indiana 47907

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B35146

Reference29 articles.

1. THE EXPLANATION OF CERTAIN ACOUSTICAL PHENOMENA 1

2. HawthorneW. R. “Theory of Combustion Instability in Liquid Propellant Rocket Motors,” edited by CroccoL.ChengS.I., Butterworths, Interscience, London, New York, 1956, p. 200.

3. CulickF. E. C. “Unsteady Motions in Combustion Chambers for Propulsion Systems,” NATO RTO-AG-AVT-039, AGARDograph, 2006.

4. PoinsotT.VeynanteD., Theoretical and Numerical Combustion, 3rd ed., 2011, p. 588, www.cerfacs.fr/elearning.

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