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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 by Bobby W. Sanders
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1Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet
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” 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: Median: 78
- Publisher: ➤ NASA, Scientific and Technical Information Office - For sale by the National Technical Information Service]
- Publish Date: 1980
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“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 Identifiers:
- The Open Library ID: OL18019834M - OL15248957M - OL17542889M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find 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 at online marketplaces:
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2Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet
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” 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: Median: 78
- Publisher: ➤ NASA, Scientific and Technical Information Office - For sale by the National Technical Information Service]
- Publish Date: 1980
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“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 Identifiers:
- The Open Library ID: OL17979273M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find 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 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
3Turbojet-exhaust-nozzle secondary-airflow pumping as an exit control of an inlet-stability bypass system for a Mach 2.5 axisymmetric mixed-compression inlet
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” 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: Median: 78
- Publisher: ➤ NASA, Scientific and Technical Information Office - For sale by the National Technical Information Service]
- Publish Date: 1980
- Publish Location: ➤ Washington, D.C - [Springfield, Va
“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 Identifiers:
- The Open Library ID: OL14932495M
Access and General Info:
- First Year Published: 1980
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find 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 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
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- Ebay: New and used books.