Numerical Simulations of a Single Injector Gaseous Methane Rocket Combustion Chamber (AIAA 2016-2148)
Aerospace sciences meeting
2016-01-01
14 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DataCite | 1886
A High-Order Immersed-Boundary Method for Simulations of Flapping Wings (AIAA 2014-2148)
British Library Conference Proceedings | 2014
|Design Procedure of a Movable Pintle Injector for Liquid Rocket Engines (AIAA 2016-1453)
British Library Conference Proceedings | 2016
|