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
Title:
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
Author:
Sanders, Bobby W.
Personal Author:
Publication Information:
Washington, D.C. : NASA, Scientific and Technical Information Office ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1980.
Physical Description:
iii, 78 pages : illustrations ; 27 cm.
General Note:
"Lewis Research Center."
"January 1980"--Cover.
Language:
English
Subject Term:
Format :
Book