Film cooling on the pressure surface of a turbine vane

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040 ‡aGPO ‡cGPO ‡dABC ‡dOCLCQ
049 ‡aUIUU
050 4 ‡aTL521.3.T4 ‡bA3 no. 3536
086 0 ‡aNAS 1.15:X-3536
100 1 ‡aGauntner, James W.
245 1 0 ‡aFilm cooling on the pressure surface of a turbine vane / ‡cJames W. Gauntner and Herbert J. Gladden ; Lewis Research Center.
260 ‡aWashington : ‡bNational Aeronautics and Space Administration ; ‡aSpringfield, Va. : ‡bFor sale by National Technical Information Service, ‡c1977.
300 ‡a16 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical memorandum ; ‡vNASA TM X-3536
500 ‡aIssued May 1977.
504 ‡aIncludes bibliographical references.
538 ‡aMode of access: Internet.
650 0 ‡aGas-turbines ‡xCooling.
700 1 ‡aGladden, Herbert J., ‡ejoint author.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration.
CID ‡a011426064
DAT 0 ‡a20101006154422.0 ‡b20141013010000.0
DAT 1 ‡a20141112173021.0 ‡b2023-03-14T18:28:07Z
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