Experimental program conducted at Pratt and Whitney Aircraft Div and wind tunnel test data obtained during comprehensive study of supersonic pod to pod inlet interference; test established, for typical Mach 3.0 design mixed compression inlet, dividing line between regions of expelled shock interference and completely stable operation and total pressure recovery penalty imposed by operating with pod to pod interference; penalty required to maintain stability during initial transient of onset of "buzz" was so severe that it cannot be considered practical; plate placed between pods was found to be very effective in eliminating interference penalty.
Experimental investigation of inlet-to-inlet shock interference
SAE -- Paper
SAE Meeting ; 1965 Inlets
1965
17 pages
Conference paper
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Experimental Investigation of Inlet-to-Inlet Shock Interference
SAE Technical Papers | 1965
|Inlet-to-inlet shock interference tests
TIBKAT | 1965
|Inlet-to-inlet shock interference tests
Engineering Index Backfile | 1965
|Inlet-to-inlet shock interference tests final report
NTRS | 1965
|Inlet-TO-Inlet Shock Interference Tests Final Report
NTIS | 1965
|