Two-dimensional cold-air cascade study of a film-cooled turbine stator blade : IV, comparison of experimental and analyatical aerodynamic results for blade with 12 rows of 0.076-centimeter (0.030-in.-) diameter holes having streamwise ejection angles

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040 ‡aGPO ‡cGPO ‡dOCL
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050 4 ‡aTL521.3 ‡b.T4 nos.1146-1159
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086 0 ‡aNAS 1.60:1151
100 1 ‡aPrust, Herman W.
245 1 0 ‡aTwo-dimensional cold-air cascade study of a film-cooled turbine stator blade : ‡bIV, comparison of experimental and analyatical aerodynamic results for blade with 12 rows of 0.076-centimeter (0.030-in.-) diameter holes having streamwise ejection angles / ‡cHerman W. Prust, Jr. ; Lewis Research Center.
260 ‡a[Washington] : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office ; ‡aSpringfield, Va. : ‡bfor sale by the National Technical Information Service, ‡c1978.
265 ‡a22161
300 ‡a27 p. : ‡bill. ; ‡c27 cm.
490 0 ‡aNASA technical paper ; ‡v1151
500 ‡aIssued Mar. 1978.
504 ‡aIncludes bibliographical references.
538 ‡aMode of access: Internet.
650 0 ‡aTurbines ‡xBlades.
710 2 ‡aLewis Research Center.
710 1 ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Office.
CID ‡a011426207
DAT 0 ‡a20101007083812.0 ‡b20141013010000.0
DAT 1 ‡a20141112173021.0 ‡b2023-03-14T18:16:11Z
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