Effects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0

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086	0	⊔	‡aNAS 1.15:X-374
100	1	⊔	‡aAhtye, Warren F.
245	1	0	‡aEffects of wing incidence on the longitudinal trim characteristics of a cambered 70° delta-wing configuration at mach numbers 3.0 to 5.0 / ‡cby Warren F. Ahtye.
246	3	⊔	‡aEffects of wing incidence on the longitudinal trim characteristics of a cambered 70 degree delta-wing configuration at mach numbers 3.0 to 5.0
260	⊔	⊔	‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, ‡c1960.
300	⊔	⊔	‡a52 p. : ‡bill. ; ‡c26 cm.
490	0	⊔	‡aNASA technical memorandum ; ‡vX-374
500	⊔	⊔	‡a"September 1960."
500	⊔	⊔	‡aCover title.
504	⊔	⊔	‡aIncludes bibliographical references (p. 23).
530	⊔	⊔	‡aFull text also available online. Address as of 11/15/2010: ‡uhttp://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19650003202_1965003202.pdf.
538	⊔	⊔	‡aMode of access: Internet.
650	⊔	0	‡aFighter planes ‡xSafety measures ‡xTesting.
650	⊔	0	‡aStability of airplanes, Longitudinal ‡xTesting.
650	⊔	0	‡aAirplanes ‡xWings, Triangular ‡xTesting.
650	⊔	0	‡aDelta wing airplanes ‡xStability ‡xTesting.
710	2	⊔	‡aAmes Research Center.
CID	⊔	⊔	‡a011446636
DAT	0	⊔	‡a20101115131852.0 ‡b20141009010000.0
DAT	1	⊔	‡a20141112165512.0 ‡b2025-01-01T18:56:46Z
DAT	2	⊔	‡a2025-01-01T18:30:02Z
CAT	⊔	⊔	‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
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