Jet effects on longitudinal trim of an airplane configuration measured at mach numbers between 1.2 and 1.8

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040 ‡aAD# ‡cAD#
041 0 ‡aeng
049 ‡aUIUU
086 0 ‡aNAS 1.14:D-177
088 ‡aNASA-TN-D-177
100 0 ‡aPeck, Robert F.
245 1 0 ‡aJet effects on longitudinal trim of an airplane configuration measured at mach numbers between 1.2 and 1.8 / ‡cby Robert F. Peck.
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration : ‡b[For sale by the Office of Technical Services, Dept. of Commerce], ‡c[1959]
300 ‡a17 p. : ‡bill. ; ‡c26 cm.
490 0 ‡aNASA technical note ; ‡vNASA TN D-177
500 ‡aCover title.
500 ‡a"December 1959."
500 ‡aFlow, jet-mixing; Exits; Airplanes, components in combination; Interference, jet-missiles; Stability, longitudinal-static; Stability, lateral and directional, dynamic; Loads, aerodynamic, tail,
500 ‡aSupersedes NACA RM L54J29a.
504 ‡aIncludes bibliographical references.
538 ‡aMode of access: Internet.
650 7 ‡aLoads, aerodynamic, tail. ‡2nasat
650 7 ‡aStability, lateral and directional, dynamic. ‡2nasat
650 7 ‡aStability, longitudinal-static. ‡2nasat
650 7 ‡aInterference, jet-missiles. ‡2nasat
650 7 ‡aAirplanes, components in combination. ‡2nasat
650 7 ‡aExits. ‡2nasat
650 7 ‡aFlow, jet-mixing. ‡2nasat
710 2 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011446912
DAT 0 ‡a20101105142217.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2023-03-14T18:18:20Z
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FMT ‡aBK
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