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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Bibliographic Details
Main Author: Shaw, Robert J (Robert Joseph), 1946-
Corporate Author: Lewis Research Center
Other Authors: Mitchell, Glenn A, Sanders, Bobby W
Format: Government Document Book
Language:English
Published: 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
Subjects:
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