Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet/
| Main Author: | |
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| Corporate Authors: | , , |
| Format: | Book |
| Language: | English |
| Published: |
Washington, D.C.:
NASA, Scientific and Technical Information Office,
1980
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| Series: | NASA technical paper
1532 |
| Subjects: |