Suppressing Restricted Shock Separation in Thrust-Optimized Rocket Nozzles Using Contour Geometry (AIAA 2015-4220)
Joint propulsion conference
01.01.2015
22 pages
Aufsatz (Konferenz)
Englisch
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Suppressing Restricted Shock Separation in a Subscale Rocket Nozzle Using Contour Geometry
Online Contents | 2016
|Suppressing Restricted Shock Separation in a Subscale Rocket Nozzle Using Contour Geometry
Online Contents | 2016
|