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 eBook
Language:	English
Published:	Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
Series:	NASA technical paper ; 1531.
Subjects:	Airplanes > Turbojet engines > Air intakes. Airplanes > Motors > Valves. Aerodynamic stability. Bypasses. Propulsion system performance. Supersonic inlets. Turbojet engines. Wind tunnel stability tests.
Online Access:	https://purl.fdlp.gov/GPO/gpo52217

Description
Item Description:	Title from title screen (viewed Sept. 22, 2014). "January 1980." "Performing organization, Lewis Research Center"--Technical report documentation page.
Physical Description:	1 online resource (iii, 98 pages) : illustrations.
Bibliography:	Includes bibliographical references (pages 27-28).