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 / Bobby W. Sanders.
Series InformationNASA technical paper
- Physical Description: 1 online resource (iii, 98 pages) : illustrations.
- Publisher: Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
Title from title screen (viewed Sept. 22, 2014).
"Performing organization, Lewis Research Center"--Technical report documentation page.
|Bibliography, etc. Note:||
Includes bibliographical references (pages 27-28).
|Funding Information Note:||
Sponsored by National Aeronautics and Space Administration 505-04
Search for related items by subject
|Subject:||Airplanes > Turbojet engines > Air intakes.
Airplanes > Motors > Valves.