Cold-air annular-cascade investigation of aerodynamic performance of core-engine-cooled turbine vanes : II--Pressure surface trailing edge ejection and split trailing edge ejection /
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington : Springfield, Va. :
U.S. National Aeronautics and Space Administration ; for sale by the National Technical Information Service,
1976
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| Series: | NASA technical memorandum ;
NASA TM X-3369 |
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Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Johns Hopkins University
| Call Number: |
NASA TM X3369 |
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