2 edition of Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients found in the catalog.
Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controled inlet-stability bypass system when subjected to internal and external airflow transients
Bobby W Sanders
by National Aeronautics and Space Administration, Scientific and Technical Information Office, For sale by the National Technical Information Service] in Washington, D.C, [Springfield, Va
Written in English
|Statement||Bobby W. Sanders|
|Series||NASA technical paper -- 1531|
|Contributions||United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lewis Research Center|
|The Physical Object|
|Pagination||iii, 98 p. :|
|Number of Pages||98|
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