NASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel

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050 4 ‡aTL521.3 ‡b.N18 no.2890
086 0 ‡aNAS 1.60:2890
100 1 ‡aJenkins, Renaldo V.
245 1 0 ‡aNASA SC(2)-0714 airfoil data corrected for sidewall boundary-layer effects in the Langley 0.3-meter transonic cryogenic tunnel / ‡cRenaldo V. Jenkins.
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, ‡c1989.
300 ‡a55 p. : ‡bill. ; ‡c28 cm.
490 0 ‡aNASA technical paper ; ‡v2890
500 ‡a"March 1989"--Cover.
504 ‡aIncludes bibliographical references (p. 5-6).
538 ‡aMode of access: Internet.
650 0 ‡aWind tunnels.
650 0 ‡aReynolds number.
650 0 ‡aBoundary layer.
650 0 ‡aAerofoils.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bOffice of Management.
CID ‡a011423010
DAT 0 ‡a20100928125333.0 ‡b20141013010000.0
DAT 1 ‡a20141112173021.0 ‡b2025-01-01T19:20:46Z
DAT 2 ‡a2025-01-01T18:30:02Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
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