Distributed educated throat stability bypass to increase the stable airflow range of a Mach 2.5 inlet with 60-percent internal contraction /
The results of an experimental investigation to increase the stable airflow operating range of a supersonic mixed-compression inlet are presented. A distributed educated throat stability-bypass entrance configuration was tested. In terms of diffuser-exit corrected airflow, a large inlet stable airfl...
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| Format: | Government Document Book |
| Language: | English |
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Washington, D.C. : Springfield, Va. :
National Aeronautics and Space Administration ; For sale by the National Technical Information Service [distributor],
1974
Washington, D.C. : [Springfield, Va. : National Aeronautics and Space Administration ; For sale by the National Technical Information Service], 1974 |
| Series: | NASA technical memorandum ;
2975 NASA technical memorandum X-2975 |
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