Application of oblique-shock sensing system to ram-jet-engine flight Mach number control

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050	⊔	4	‡aTL709.5.C57 ‡bW55 1955
086	0	⊔	‡aY 3.N21/5:15/E54L22a
100	1	⊔	‡aWilcox, Fred A.
245	1	0	‡aApplication of oblique-shock sensing system to ram-jet-engine flight Mach number control / ‡cby Fred A. Wilcox and Donald P. Hearth.
260	⊔	⊔	‡aWashington [D.C.] : ‡bNational Aeronautics and Space Administration, ‡c[1955]
300	⊔	⊔	‡a29 p. : ‡bill. ; ‡c27 cm.
490	0	⊔	‡aNACA research memorandum ; ‡vE54L22a
500	⊔	⊔	‡a"Declassified February 10, 1959."
500	⊔	⊔	‡a"March 3, 1955."
500	⊔	⊔	‡aCover title.
504	⊔	⊔	‡aIncludes bibliographical reference (p. 10-11).
538	⊔	⊔	‡aMode of access: Internet.
650	⊔	0	‡aAerodynamics, Supersonic.
650	⊔	0	‡aAirplanes ‡xRamjet engines ‡xDiffusers ‡xTesting.
650	⊔	0	‡aAirplanes ‡xRamjet engines ‡xControl systems ‡xTesting.
700	1	⊔	‡aHearth, Donald P.
710	2	⊔	‡aLewis Flight Propulsion Laboratory.
710	2	⊔	‡aUnited States. ‡bNational Adviosry Committee for Aeronautics. ‡tNACA research memorandum.
710	1	⊔	‡aUnited States. ‡bNational Aeronautics and Space Administration.
730	0	⊔	‡aTechnical Report Archive & Image Library (TRAIL)
899	⊔	⊔	‡a39015086463547
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