A free-flight investigation at high subsonic and low supersonic speeds of the rolling effectiveness and drag of three spoiler controls having potentially low actuating-force requirements

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049 ⊔ ⊔ ‡aNACA
086 0 ⊔ ‡aY 3.N21/5:15/L55G11a
100 1 ⊔ ‡aSchult, Eugene D.
245 1 2 ‡aA free-flight investigation at high subsonic and low supersonic speeds of the rolling effectiveness and drag of three spoiler controls having potentially low actuating-force requirements / ‡cby Eugene D. Schult.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1955.
300 ⊔ ⊔ ‡a35 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNACA research memorandum ; ‡vL55G11a
500 ⊔ ⊔ ‡a"September 20, 1955; Declassified May 29, 1959."
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 16).
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aDrag (Aerodynamics)
650 ⊔ 0 ‡aRolling (Aerodynamics)
650 ⊔ 0 ‡aAirplanes ‡xControl systems.
650 ⊔ 0 ‡aSpoilers (Airplanes)
710 2 ⊔ ‡aLangley Aeronautical Laboratory.
710 1 ⊔ ‡aUnited States. ‡bNational Adviosry Committee for Aeronautics. ‡tNACA research memorandum.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
899 ⊔ ⊔ ‡a39015086507053
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