Numerical Simulations of a Single Injector Gaseous Methane Rocket Combustion Chamber (AIAA 2016-2148)
Aerospace sciences meeting
01.01.2016
14 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
AN OVERVIEW OF COMBUSTION INSTABILITIES AND ROCKET ENGINE INJECTOR DESIGN (AIAA 2016-4724)
British Library Conference Proceedings | 2016
|CHARACTERIZATION OF A MULTI-INJECTOR GOX/CH4 COMBUSTION CHAMBER (AIAA 2016-4992)
British Library Conference Proceedings | 2016
|DataCite | 1886
A High-Order Immersed-Boundary Method for Simulations of Flapping Wings (AIAA 2014-2148)
British Library Conference Proceedings | 2014
|