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Bobby W. Sanders

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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

by Bobby W. Sanders First published in 1980
3 editions

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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

by Bobby W. Sanders First published in 1980
1 edition

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OLID: OL4830103A

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