Experimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet

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100 1 ⊔ ‡aCole, Henry A. ‡cJr.
245 1 0 ‡aExperimental and predicted longitudinal response characteristics of a large flexible 35 degree swept-wing airplane at an altitude of 35,000 feet / ‡cby Henry A. Cole, Jr., Stuart C. Brown, and Euclid C. Holleman.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Advisory Committee for Aeronautics, ‡c[1954].
300 ⊔ ⊔ ‡a63 p. : ‡bill. ; ‡c27 cm.
490 0 ⊔ ‡aNational Advisory Committee for Aeronautics research memorandum ; ‡vA54H09
500 ⊔ ⊔ ‡aOn front cover: "November 26, 1954."
504 ⊔ ⊔ ‡aIncludes bibliographical references: p. 32-33.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAirplanes ‡xWings ‡xTesting.
650 ⊔ 0 ‡aAirplanes ‡xWings, Swept-back.
650 ⊔ 0 ‡aAeronautics ‡xResearch.
700 1 ⊔ ‡aHolleman, Euclid C., ‡ejoint author.
700 1 ⊔ ‡aBrown, Stuart C., ‡d1938- ‡ejoint author.
710 1 ⊔ ‡aUnited States. ‡bNational Advisory Committee for Aeronautics. ‡tNACA research memorandum.
710 2 ⊔ ‡aAmes Research Center.
730 0 ⊔ ‡aTechnical Report Archive & Image Library (TRAIL)
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CID ⊔ ⊔ ‡a100167691
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DAT 1 ⊔ ‡a20220603140513.0 ‡b2024-04-20T17:42:50Z
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