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 - Info and Reading Options
By Bobby W. Sanders
"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" was published by National Aeronautics and Space Administration, Scientific and Technical Information Office in 1980 - Washington, D.C, it has 98 pages and the language of the book is English.
“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” Metadata:
- Title: ➤ 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
- Author: Bobby W. Sanders
- Language: English
- Number of Pages: 98
- Publisher: ➤ National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1980
- Publish Location: Washington, D.C
“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” Subjects and Themes:
- Subjects: ➤ Airplanes - Turbojet engines - Air intakes - Motors - Valves - Aerodynamic stability - Bypasses - Propulsion system performance - Supersonic inlets - Wind tunnel stability tests
Edition Specifications:
- Pagination: ➤ 1 online resource (iii, 98 pages)
Edition Identifiers:
- The Open Library ID: OL43506459M - OL31808657W
- Online Computer Library Center (OCLC) ID: 761221787
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