Effect of velocity and temperature distribution at the hole exit on film cooling of turbine blades
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| Format: | Government Document Book |
| Language: | English |
| Published: |
[Washington, D.C. : Springfield, Va. :
National Aeronautics and Space Administration ; National Technical Information Service, distributor,
1997]
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| Series: | NASA technical memorandum
208146 |
| Subjects: |
Internet
This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.Stanford University
| Call Number: |
ISIL:US-CST NAS 1.15:208146 |
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