A preliminary investigation of the pressure recovery of several two-dimensional supersonic inlets at Mach number of 2.01 Page: 1 of 30
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A PRELIMINARY INVESTIGATION OF TEE PRESSURE RECOVERY OF
SEVERAL TWO-DIMENSIONAL SUPERSONIC INLETS
AT A MACH NUMBER OF 2.01
By Raymond J. Comenzo
Langley Aeronautical Laboratory
Langley Field, Va.
This material contains nformatIoa a ecting the national Defense of the United States within the meaning
of the espionage laws, Title 18, U.S.C., Sees. ?93 and 794, the transmission or revelatlo of which in any
maner to an unauthorized person is prohibited by law.
NATIONAL ADVISORY COMMITTEE
June 23, 1954
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Comenzo, Raymond J. A preliminary investigation of the pressure recovery of several two-dimensional supersonic inlets at Mach number of 2.01, report, June 23, 1954; (digital.library.unt.edu/ark:/67531/metadc60464/m1/1/: accessed June 21, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.