Transonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail

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049 ‡aNACA
086 0 ‡aY 3.N21/5:15/L54K19a
100 1 ‡aHieser, Gerald.
245 1 0 ‡aTransonic longitudinal aerodynamic characteristics of a fighter-type airplane model with a low-aspect-ratio unswept wing and tee-tail / ‡cby Gerald Hieser and Charles F. Reid, Jr.
260 ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c1956.
300 ‡a58 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNational Advisory Committee for Aeronautics research memorandum ; ‡vL54K19a
500 ‡a"October 15, 1956."
504 ‡aIncludes bibliographical references (p. 17-18).
538 ‡aMode of access: Internet.
650 0 ‡aAerodynamics, Transonic.
650 0 ‡aAirplanes ‡xTail surfaces.
650 0 ‡aAirplanes ‡xBrakes.
650 0 ‡aAspect ratio (Aerofoils)
650 0 ‡aStability of airplanes, Longitudinal.
700 1 ‡aReid, Charles F.
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 ‡a39015086490409
CID ‡a100168583
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DAT 1 ‡a20221207060734.0 ‡b2024-03-16T17:40:20Z
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