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Feasibility study of inlet shock stability system of YF-12The feasibility of self actuating bleed valves as a shock stabilization system in the inlet of the YF-12 is considered for vortex valves, slide valves, and poppet valves. Analytical estimation of valve performance indicates that only the slide and poppet valves located in the inlet cowl can meet the desired steady state stabilizing flows, and of the two the poppet valve is substantially faster in response to dynamic disturbances. The poppet valve is, therefore, selected as the best shock stability system for the YF-12 inlet.
Document ID
19760024107
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Blausey, G. C.
(Lockheed Aircraft Corp. Burbank, CA, United States)
Coleman, D. M.
(Lockheed Aircraft Corp. Burbank, CA, United States)
Harp, D. S.
(Lockheed Aircraft Corp. Burbank, CA, United States)
Date Acquired
September 3, 2013
Publication Date
November 17, 1972
Subject Category
Aerodynamics
Report/Patent Number
SP-1964
NASA-CR-134594
Report Number: SP-1964
Report Number: NASA-CR-134594
Accession Number
76N31195
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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