Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet - Info and Reading Options
By Bobby W. Sanders
"Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet" was published by NASA, Scientific and Technical Information Office in 1980 - Washington, D.C, it has 78 pages and the language of the book is English.
“Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet” Metadata:
- Title: ➤ Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet
- Author: Bobby W. Sanders
- Language: English
- Number of Pages: 78
- Publisher: ➤ NASA, Scientific and Technical Information Office
- Publish Date: 1980
- Publish Location: Washington, D.C
“Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet” Subjects and Themes:
- Subjects: Air intakes - Airplanes - Turbojet engines
Edition Specifications:
- Pagination: iii, 78 p. :
Edition Identifiers:
- The Open Library ID: OL17542889M - OL11473289W
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