Method of determining reduction in elevator effectiveness when engine is mounted on aft fuselage of aircraft

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040 ‡aTRAAL ‡beng ‡cTRAAL
049 ‡aMAIN
086 0 ‡aD 301.45/13: 61-52
100 1 ‡aAtchison, James R., ‡eauthor.
245 1 0 ‡aMethod of determining reduction in elevator effectiveness when engine is mounted on aft fuselage of aircraft / ‡cJames R. Atchison.
264 1 ‡aWright-Patterson Air Force Base, Ohio : ‡bAeronautical Systems Division, Air Force Systems Command, United States Air Force, ‡c1961.
300 ‡avi, 11 pages : ‡billustrations, figures, tables ; ‡c28 cm.
336 ‡atext ‡btxt ‡2rdacontent
337 ‡aunmediated ‡bn ‡2rdamedia
338 ‡avolume ‡bnc ‡2rdacarrier
490 0 ‡aWADD-TN ; ‡v61-52
500 ‡a"The report was initiated by the Stability and Control Branch, Flight Dynamics Divisoin, Directorate of Defense and Transport Systems Engineering, Aeronautical Systems Division, under System 659A."
500 ‡a"The courtesy of the Ronald Press Company and the McGraw-Hill Book Company, Inc., in granting permission to use their material in this technical report is gratefully acknowledged."
500 ‡a"July 1961."
504 ‡aIncludes bibliographical references (page 11)
533 ‡aPrint reproduction.
538 ‡aMode of access: Internet.
650 0 ‡aAirplanes ‡xFuselage.
650 0 ‡aAirplanes ‡xTurbojet engines ‡xControl systems.
710 2 ‡aAir Force Flight Dynamics Laboratory (U.S.), ‡esponsor.
710 1 ‡aUnited States. ‡bAir Force. ‡bSystems Command, ‡eissuing agency.
710 1 ‡aUnited States. ‡bAir Force. ‡bSystems Command. ‡bAeronautical Systems Division, ‡esponsor.
730 0 ‡aTechnical Report Archive & Image Library (TRAIL)
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DAT 1 ‡a20241209061151.0 ‡b2024-12-09T14:47:07Z
DAT 2 ‡a2024-07-30T17:30:02Z
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