Shock position control for mode transition in a turbine based combined cycle engine inlet model /
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| Main Authors: | , |
|---|---|
| Corporate Author: | |
| Format: | Government Document Electronic eBook |
| Language: | English |
| Published: |
Cleveland, Ohio :
National Aeronautics and Space Administration, Glenn Research Center,
2013.
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| Series: | NASA technical memorandum ;
217824. |
| Subjects: | |
| Online Access: | CONNECT |
