Effect of cooling-hole geometry on aerodynamic performance of a film-cooled turbine van tested with cold air in a two-dimensional cascade /
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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
1136 |
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