Investigation of Drag and Pressure Recovery of a Scoop Inlet in the Transonic Speed Range Page: 1 of 39
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RM A52F27DEC 19 1952
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aRESEARCH MEMORANDUM
INVESTIGATION OF DRAG AND PRESSURE RECOVERY OF A
SCOOP INLET IN THE TRANSONIC SPEED RANGE
By James Selna, Loren G. Bright,
and Bernard A. Schlaff
Ames Aeronautical Laboratory
Moffett Field, Calif.
CLASSIFICATION CANCELLED
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CLOW=1 DOCUMENT
Ths mara contalm information effctis the ?ationsl Defense of th united Sateh witLn the snI
of the epioa ge law Tl 18, U.S.C., Sees. 79 sa i79, the trammiatcn or revelton f which in any
maer to aunz red person is probibtad law.
NATIONAL ADVISORY COMMITTEE
FOR AERONAUTICSWASHINGTON
December 15, 1962UNCLASSIFIED
Ch{FIDE NTIAL NACA LIBRARY
LANGLEY AERONAUTK.AL LABORAISRt
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Selna, James; Bright, Loren G. & Schlaff, Bernard A. Investigation of Drag and Pressure Recovery of a Scoop Inlet in the Transonic Speed Range, report, December 15, 1952; (https://digital.library.unt.edu/ark:/67531/metadc59321/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.