An adverse effect of film cooling on the suction surface of a turbine vane

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035 ‡asdr-uiuc6406398
035 ‡a(OCoLC)25740026
040 ‡aABC ‡cABC
049 ‡aUIUU
050 4 ‡aTL521 ‡b.A3525 no. 7618
100 1 ‡aGladden, Herbert J.
245 1 3 ‡aAn adverse effect of film cooling on the suction surface of a turbine vane / ‡cby Herbert J. Gladden and James W. Gauntner.
260 ‡aWashington, D.C. : ‡bNational Aeronautics and Space Administration ; ‡a[Springfield, Va. : ‡bFor sale by the National Technical Information Service], ‡c1974.
300 ‡a24 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical note ; ‡vNASA TN D-7618
500 ‡aPrepared at Lewis Research Center.
500 ‡aCover title.
504 ‡aIncludes bibliographical references (p. 12-13).
538 ‡aMode of access: Internet.
650 0 ‡aTurbines ‡xBlades ‡xCooling.
700 1 ‡aGauntner, James W.
710 2 ‡aLewis Research Center.
CID ‡a011447251
DAT 0 ‡a20101111150254.0 ‡b20141009010000.0
DAT 1 ‡a20141112165512.0 ‡b2024-01-26T18:53:44Z
CAT ‡aSDR-UIUC ‡dUNKNOWN ‡lloader.pl-003-020
FMT ‡aBK
HOL ‡0sdr-uiuc6406398 ‡auiug ‡bSDR ‡cUIUC ‡puiug.30112106642520 ‡sUIU ‡16406398
974 ‡bUIU ‡cUIUC ‡d20240126 ‡sgoogle ‡uuiug.30112106642520 ‡y1974 ‡rpd ‡qbib ‡tUS fed doc--NTIS: pubdate < 2019