Effects of a J34 Turbojet Engine on Supersonic Diffuser Performance
Description:
Report presenting testing of a translating cone inlet with a variable bypass at Mach numbers 1.6, 1.8, and 2.0 with both a choked exit plug and a J34 turbojet engine. The main difference between the two options was increased inlet subcritical stability with the engine. Results regarding basic diffuser performance, inlet stability, buzz amplitude and frequency, and diffuser-exit profiles are provided.
Date:
January 4, 1956
Creator:
Beheim, Milton A. & Englert, Gerald W.
Item Type:
Refine your search to only
Report