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
Title:
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
Author:
Sanders, Bobby W.
Personal Author:
Publication Information:
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1980.
Physical Description:
iii, 98 pages : illustrations ; 27 cm.
General Note:
"Lewis Research Center."
"January 1980"--Cover.
Language:
English
Format :
Book