Limited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration

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035 ‡a(OCoLC)8961245
040 ‡aGPO ‡cGPO ‡dABC
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050 4 ‡aTL521.3.T4 ‡bA3 no. 81972
074 ‡a830-D (microfiche)
086 0 ‡aNAS 1.15:81972
100 1 ‡aKelley, Wendell W.
245 1 0 ‡aLimited evaluation of an F-14A airplane utilizing an aileron-rudder inter-connect control system in the landing configuration / ‡cWendell W. Kelley, Einar K. Enevoldson.
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Branch ; ‡a[Springfield, Va. ‡bFor sale by the National Technical Information Service], ‡c1981.
300 ‡a36 p. : ‡bill. ; ‡c28 cm.
490 0 ‡aNASA technical memorandum ; ‡v81972
500 ‡a"December 1981"--Cover.
500 ‡a"Dryden Flight Research Center."
500 ‡a"Langley Research Center."
504 ‡aIncludes bibliographical references.
538 ‡aMode of access: Internet.
650 0 ‡aAirplanes ‡xControl systems.
650 0 ‡aAirplanes, Military ‡xFlight testing.
650 0 ‡aAilerons.
700 1 ‡aEnevoldson, Einar K.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Branch.
710 2 ‡aHugh L. Dryden Flight Research Center.
710 2 ‡aLangley Research Center.
CID ‡a011426920
DAT 0 ‡a20101008160403.0 ‡b20141013010000.0
DAT 1 ‡a20141112173021.0 ‡b2024-10-10T18:05:26Z
DAT 2 ‡a2024-10-10T17:30:01Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
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