Shock tunnel studies of scramjet phenomena

final technical report, NAGW-674.

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1996

Publisher

National Aeronautics and Space Administration,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Shock tunnels, Supersonic combustion ramjet engines, Data acquisition, Enthalpy, Investigation, Thrust, Hypersonic nozzles, Mach number