https://catalogue-scientifique.canada.ca/record=2232894~S6*frc
Rechercher Eramya, Allen; Rechercher Gimelshein, Sergey; Rechercher Cline, Jason; Rechercher Braunstein, Matthew
air force research lab edwards afb ca propulsion directorate, 2007
The direct simulation Monte Carlo method is used to model a transient stage separation of a generic sounding rocket at 100 km. Lower stage movement is...
Publication gouvernementale