Influence of fuselage-mounted rocket boosters on flow field at inlet and on diffuser performance of strut-mounted engine at Mach numbers of 1.8 and 2.0
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SECURITY Y INJFORIA'TION Copy33 RM E52IOZ RESEARCH MEMORANDUM FIELD AT INLET AND ON DIFFUSER PERFORMANCE OF STRUT-MOUNTED ENGINE AT M4ACH NUMBERS OF 1.8 and 2.0 By George A. Wise and Leonard T. Obery Lewis Flight Propulsion Laboratory Cleveland, Ohio CLASSIFIED DOCUMENT , This material contain information affecting the Ntioa m l Defense a t he within the of the espionage laws, Title 18, U.S.C., Bees. 793 d 794, the vasmasion = or of which in any mp r to uautherised person is prMhibiteK by law. NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS ! WASHINGTON SI October 29, 1952
Wise, George A. & Obery, Leonard J.Influence of fuselage-mounted rocket boosters on flow field at inlet and on diffuser performance of strut-mounted engine at Mach numbers of 1.8 and 2.0,
report,
October 29, 1952;
(https://digital.library.unt.edu/ark:/67531/metadc59363/m1/1/:
accessed April 23, 2024),
University of North Texas Libraries, UNT Digital Library, https://digital.library.unt.edu;
crediting UNT Libraries Government Documents Department.
