Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings

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035 ⊔ ⊔ ‡asdr-uiuc6384034
035 ⊔ ⊔ ‡a(OCoLC)35827621
040 ⊔ ⊔ ‡aABC ‡cABC
049 ⊔ ⊔ ‡aUIUU
050 ⊔ 4 ‡aTL521.3.C6 ‡bA3 no. 2599
086 0 ⊔ ‡aNAS 1.26:2599
100 1 ⊔ ‡aWeatherill, W. H.
245 1 0 ‡aComputation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings / ‡cWarren H. Weatherill, F. Edward Ehlers, and James D. Sebastian.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service, ‡c1975]
300 ⊔ ⊔ ‡avi, 150 p.: ‡bill. ; ‡c27 cm.
490 ⊔ 0 ‡aNASA contractor report ; ‡vNASA CR-2599
500 ⊔ ⊔ ‡a"Prepared by the Boeing Commercial Airplane Company ... for Langley Research Center."
500 ⊔ ⊔ ‡a"December 1975."
500 ⊔ ⊔ ‡aCover title.
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 149-150).
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aUnsteady flow (Aerodynamics) ‡xComputer simulation.
650 ⊔ 0 ‡aOscillating wings (Aerodynamics) ‡xComputer simulation.
650 ⊔ 0 ‡aAerodynamics, Transonic ‡xComputer simulation.
700 1 ⊔ ‡aSebastian, James D.
700 1 ⊔ ‡aEhlers, F. Edward.
710 2 ⊔ ‡aLangley Research Center.
710 2 ⊔ ‡aBoeing Commercial Airplane Company.
CID ⊔ ⊔ ‡a011430383
DAT 0 ⊔ ‡a20101025154700.0 ‡b20141009010000.0
DAT 1 ⊔ ‡a20141112164151.0 ‡b2025-01-01T18:38:17Z
DAT 2 ⊔ ‡a2025-01-01T18:30:02Z
CAT ⊔ ⊔ ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ⊔ ⊔ ‡aBK
HOL ⊔ ⊔ ‡0sdr-uiuc6384034 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112101595863 ‡sUIU ‡16384034
974 ⊔ ⊔ ‡bUIU ‡cUIUC ‡d20250101 ‡sgoogle ‡uuiug.30112101595863 ‡y1975 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019