Design guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations

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035 ⊔ ⊔ ‡asdr-uiuc6361246
035 ⊔ ⊔ ‡a(OCoLC)502141677
040 ⊔ ⊔ ‡aCSL ‡cTEF
049 ⊔ ⊔ ‡aUIUU
050 ⊔ 4 ‡aTL672 ‡b.S67 1959
100 1 ⊔ ‡aSpreemann, Kenneth P.
245 1 0 ‡aDesign guide for pitch-up evaluation and investigation at high subsonic speeds of possible limitations due to wing-aspect-ratio variations / ‡cby Kenneth P. Spreemann.
260 ⊔ ⊔ ‡aWashington [D.C.] : ‡bNational Aeronautics and Space Administration, ‡c[1959]
300 ⊔ ⊔ ‡a37 p. : ‡b15 ill. ; ‡c27 cm.
490 0 ⊔ ‡aNASA technical memorandum ; ‡vX-26
500 ⊔ ⊔ ‡a"August 1959."
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 14-16).
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAirplanes, Tailless.
650 ⊔ 0 ‡aAirplanes ‡xTail surfaces.
650 ⊔ 0 ‡aAspect ratio (Aerofoils)
650 ⊔ 0 ‡aPitching (Aerodynamics)
650 ⊔ 0 ‡aAirplanes ‡xWings ‡xDesign and construction.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ⊔ ⊔ ‡a100233503
DAT 0 ⊔ ‡a20101005101821.0 ‡b20141009010000.0
DAT 1 ⊔ ‡a20141112165512.0 ‡b2024-01-26T18:52:38Z
CAT ⊔ ⊔ ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ⊔ ⊔ ‡aBK
HOL ⊔ ⊔ ‡0sdr-uiuc6361246 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106562777 ‡sUIU ‡16361246
974 ⊔ ⊔ ‡bUIU ‡cUIUC ‡d20240126 ‡sgoogle ‡uuiug.30112106562777 ‡y1959 ‡rpd ‡qbib ‡tUS fed doc