2 options
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.
- Format:
- Book
- Government document
- Author/Creator:
- Sanders, Bobby W., author.
- Lewis Research Center, author.
- Series:
- NASA technical paper ; 1531.
- NASA technical paper ; 1531
- Language:
- English
- Subjects (All):
- Airplanes--Turbojet engines--Air intakes.
- Airplanes.
- Airplanes--Motors--Valves.
- Genre:
- technical reports.
- Technical reports
- Technical reports.
- Physical Description:
- 1 online resource (iii, 98 pages) : illustrations.
- Place of Publication:
- Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office, January 1980.
- Notes:
- Title from title screen (viewed Sept. 22, 2014).
- "January 1980."
- "Performing organization, Lewis Research Center"--Technical report documentation page.
- Includes bibliographical references (pages 27-28).
- Other Format:
- Print version: Sanders, Bobby W. 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
- OCLC:
- 761221787
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