Computational Modeling of Instabilities in a Single-Element Rocket Combustor Using a Response Function AIAA Paper
43rd, Joint propulsion conference ; 2007 ; Cincinnati, OH
2007-01-01
3558 pages
Papers in the range 2007 5004 to 5862. Held on CD-ROM
Aufsatz (Konferenz)
Englisch
Propulsion , AIAA , ASME , SAE , ASEE
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Non-Linear Characteristics of Longitudinal Instabilities in a Model Rocket Combustor AIAA Paper
British Library Conference Proceedings | 2007
|Computational investigation on combustion instabilities in a rocket combustor
Online Contents | 2016
|