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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 /

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

Internet

https://purl.fdlp.gov/GPO/gpo52217

Available Online

Holdings details from Available Online
Call Number: NAS 1.60:1531
 
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NAS 1.60:1531 Available