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.-) (0.030-in.-) diameter holes having streamwise ejection angles /
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Corporate Authors: | , |
Format: | Government Document Book |
Language: | English |
Published: |
[Washington] : Springfield, Va. :
National Aeronautics and Space Administration, Scientific and Technical Information Office ; for sale by the National Technical Information Service,
1978
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Series: | NASA technical paper ;
1151 |
Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Duke University
Call Number: |
NAS 1.60:1151 |
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