Numerical Investigation of Flow Transition Behavior in Cold Flow Dual Bell Rocket Nozzles (AIAA 2015-4219)
Joint propulsion conference
01.01.2015
10 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Numerical Investigation of Flow Transition Behavior in Cold Flow Dual-Bell Rocket Nozzles
Online Contents | 2016
|Separation Shock Cutoff Frequency in Dual Bell Nozzles (AIAA 2015-4218)
British Library Conference Proceedings | 2015
|Flow Separation Study in Stiff Ovalized Rocket Nozzles, Part II: Numerical Approach (AIAA 2015-4154)
British Library Conference Proceedings | 2015
|