Effects of Rocket-Armament Exhaust Gas on the Performance of a Supersonic-Inlet J34-Turbojet-Engine Installation at Mach 2.0
Description:
Report presenting an investigation of the effects of rocket-armament-exhaust-gas ingestion on the performance of a supersonic-inlet J34-turbojet-engine installation at Mach 2. Rockets were fired from two different spike positions and with the engine at high or low speed. Results regarding engine air flow, temperature, and flame-out are provided.
Date:
February 20, 1956
Creator:
Beheim, Milton A. & Evans, Phillip J.
Item Type:
Refine your search to only
Report
Partner:
UNT Libraries Government Documents Department