An investigation at subsonic speeds of the longitudinal aerodynamic characteristics at angles of attach from -4° to 100° of delta-wing reentry configurations having vertically displaced and cambered wing-tip panels

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035 ⊔ ⊔ ‡asdr-uiuc6364492
035 ⊔ ⊔ ‡a(OCoLC)460939788
040 ⊔ ⊔ ‡aCSL ‡cTEF
049 ⊔ ⊔ ‡aUIUU
050 ⊔ 4 ‡aTL673.T7 ‡bS64 1961
100 1 ⊔ ‡aSpencer, Bernard.
245 1 3 ‡aAn investigation at subsonic speeds of the longitudinal aerodynamic characteristics at angles of attach from -4° to 100° of delta-wing reentry configurations having vertically displaced and cambered wing-tip panels / ‡cby Bernard Spencer,
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, ‡c1961.
300 ⊔ ⊔ ‡a33 p. : ‡bill. ; ‡c26 cm.
490 0 ⊔ ‡aNASA TM ; ‡vX-440
500 ⊔ ⊔ ‡a"February 1961."
504 ⊔ ⊔ ‡aIncludes bibliographical references (p. 7).
520 ⊔ ⊔ ‡aSubsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aSpace vehicles ‡xDesign and construction.
650 ⊔ 0 ‡aAerodynamics.
650 ⊔ 0 ‡aAirplanes ‡xWings, Triangular.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ⊔ ⊔ ‡a100233550
DAT 0 ⊔ ‡a20101007112300.0 ‡b20141009010000.0
DAT 1 ⊔ ‡a20141112165512.0 ‡b2024-01-24T18:37:02Z
CAT ⊔ ⊔ ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ⊔ ⊔ ‡aBK
HOL ⊔ ⊔ ‡0sdr-uiuc6364492 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106566570 ‡sUIU ‡16364492
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