Effects of three spanwise twist variations on the longitudinal aerodynamic characteristics of a thin 45° sweptback highly tapered wing at transonic speeds

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040 ⊔ ⊔ ‡aUIU ‡cUIU
049 ⊔ ⊔ ‡aUIUU
086 0 ⊔ ‡aNAS 1.15:X-126
100 1 ⊔ ‡aMugler, John P.
245 1 0 ‡aEffects of three spanwise twist variations on the longitudinal aerodynamic characteristics of a thin 45° sweptback highly tapered wing at transonic speeds / ‡cby John P. Mugler, Jr.
246 3 ⊔ ‡aEffects of 3 spanwise twist variations on the longitudinal aerodynamic characteristics of a thin 45 degree sweptback highly tapered wing at transonic speeds
260 ⊔ ⊔ ‡aWashington D.C. : ‡bNational Aeronautics and Space Administration, ‡c1959.
300 ⊔ ⊔ ‡a40 p. : ‡bill. ; ‡c26 cm.
490 0 ⊔ ‡aNASA technical memorandum ; ‡vX-126
500 ⊔ ⊔ ‡a"October, 1959."
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 9).
530 ⊔ ⊔ ‡aFull text also available online. Address as of 11/4/2010: ‡uhttp://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19650003091_1965003091.pdf.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aJet fighter planes ‡xWind tunnel testing.
650 ⊔ 0 ‡aTransonic wind tunnels ‡xTesting.
650 ⊔ 0 ‡aStability of airplanes, Longitudinal ‡xTesting.
650 ⊔ 0 ‡aAirplanes ‡xWings, Swept-back ‡xTesting.
710 2 ⊔ ‡aLangley Research Center.
CID ⊔ ⊔ ‡a011449539
DAT 0 ⊔ ‡a20101104121825.0 ‡b20141009010000.0
DAT 1 ⊔ ‡a20141112165512.0 ‡b2025-01-01T18:56:43Z
DAT 2 ⊔ ‡a2025-01-01T18:30:02Z
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