Investigation of a semispan tilting-propeller configuration and effects of ratio of wing chord to propeller diameter on several small-chord tilting-wing configurations at transition speeds

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035 ‡asdr-uiuc6402791
035 ‡a(OCoLC)55490249
040 ‡aEGM ‡cEGM
049 ‡aUIUU
100 1 ‡aSpreemann, Kenneth P.
245 1 0 ‡aInvestigation of a semispan tilting-propeller configuration and effects of ratio of wing chord to propeller diameter on several small-chord tilting-wing configurations at transition speeds / ‡cKenneth P. Spreemann.
246 3 ‡aNASA TN D-1815
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, ‡c1963.
300 ‡a31 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical note ; ‡vD-1815
504 ‡aIncludes bibliographical references (p. 8).
538 ‡aMode of access: Internet.
650 0 ‡aWinged aircraft.
650 0 ‡aSpace vehicles.
650 0 ‡aPropellers, Aerial.
650 0 ‡aAirplanes ‡xWings.
710 2 ‡aLangley Research Center.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011447294
DAT 0 ‡a20101110075818.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2024-01-26T18:53:03Z
DAT 2 ‡a2024-01-26T18:30:02Z ‡b2023-04-01T20:00:02Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ‡aBK
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