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Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients /

Bibliographic Details
Main Author: Sanders, Bobby W. (Author)
Corporate Author: Lewis Research Center (Author)
Format: Government Document Online Book
Published: Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
Series:NASA technical paper ; 1531.
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