Effect of winglets on a first-generation jet transport wing : III, pressure and spanwise load distributions for a semispan model at Mach 0.30

LDR 01367cam a2200313Ii 4500
001 011446208
003 MiAaHDL
005 20141009010000.0
006 m d
007 cr bn ---auaua
008 780808s1977 dcua b f000 0 eng d
035 ‡asdr-uiuc6392597
035 ‡a(OCoLC)4119148
037 ‡b22161
040 ‡aGPO ‡cGPO ‡dOCL ‡dOCLCQ ‡dISL
049 ‡aUIUU
050 4 ‡aTL507 ‡b.U565 D8478-8489
086 0 ‡aNAS 1.14:D-8478
100 1 ‡aMontoya, Lawrence C.
245 1 0 ‡aEffect of winglets on a first-generation jet transport wing : ‡bIII, pressure and spanwise load distributions for a semispan model at Mach 0.30 / ‡cLawrence C. Montoya and Peter F. Jacobs and Stuart G. Flechner ; Langley Research Center.
260 ‡aWashington : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1977.
300 ‡a100 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical note ; ‡vNASA TN D-8478
500 ‡aIssued June 1977.
504 ‡aIncludes bibliographical references.
538 ‡aMode of access: Internet.
650 0 ‡aAirplanes ‡xWings.
700 1 ‡aJacobs, Peter F., ‡ejoint author.
700 1 ‡aFlechner, Stuart G., ‡ejoint author.
710 2 ‡aLangley Research Center.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011446208
DAT 0 ‡a20101103092100.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2023-03-14T18:37:04Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ‡aBK
HOL ‡0sdr-uiuc6392597 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106911891 ‡sUIU ‡16392597
974 ‡bUIU ‡cUIUC ‡d20230314 ‡sgoogle ‡uuiug.30112106911891 ‡y1977 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2018