Theoretical pressure distributions on wings of finite span at zero incidence for mach numbers near 1

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050 ⊔ 4 ‡aTL521 ‡b.A3312 no. 88
086 1 ⊔ ‡aNAS 1.12:R-88
100 1 ⊔ ‡aAlksne, Alberta Y.
245 1 0 ‡aTheoretical pressure distributions on wings of finite span at zero incidence for mach numbers near 1 / ‡cby Alberta Y. Alksne and John R. Spreiter.
260 ⊔ ⊔ ‡aWashington, D.C. : ‡bU.S. G.P.O., ‡c1961.
300 ⊔ ⊔ ‡a47 p. : ‡bfig., tabl. ; ‡c26 cm.
490 0 ⊔ ‡aNational Aeronautics and Space Administration. Technical Report ; ‡v88
504 ⊔ ⊔ ‡aIncludes bibliographical references.
538 ⊔ ⊔ ‡aMode of access: Internet.
650 ⊔ 0 ‡aAirplanes ‡xWings.
650 ⊔ 0 ‡aAerodynamics, Transonic.
700 1 ⊔ ‡aSpreiter, John R.
710 1 ⊔ ‡aUnited States. ‡bNational Aeronautics and Space Administration.
710 2 ⊔ ‡aAmes Research Center.
CID ⊔ ⊔ ‡a011432654
DAT 0 ⊔ ‡a20101029102828.0 ‡b20141013010000.0
DAT 1 ⊔ ‡a20141112173021.0 ‡b2024-08-29T18:14:52Z
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