Explore: Convergent Nozzles
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
By Michael K. Ponton
“Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Metadata:
- Title: ➤ Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet
- Author: Michael K. Ponton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1999
- Publish Location: Hampton, Va - [Springfield, Va
“Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet” Subjects and Themes:
- Subjects: ➤ Exhaust gases - Aeroacoustics - Exhaust nozzles - Jet flow - Flow characteristics - Subsonic flow - Convergent nozzles - High Reynolds number - Engine noise - Pressure oscillations
Edition Identifiers:
- The Open Library ID: OL15550628M
Author's Alternative Names:
"Nichael K. Ponton"Access and General Info:
- First Year Published: 1999
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
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2Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
By David J. Wing
“Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct” Metadata:
- Title: ➤ Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct
- Author: David J. Wing
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1998
- Publish Location: Hampton, Va - Springfield, VA
“Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct” Subjects and Themes:
- Subjects: ➤ Pitch (Inclination) - Convergent nozzles - Flapping - Angular distribution - Thrust vector control - Nozzle geometry - Flow distribution
Edition Identifiers:
- The Open Library ID: OL15542756M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
Downloads Are Not Available:
The book is not public therefore the download links will not allow the download of the entire book, however, borrowing the book online is available.
Online Borrowing:
Online Marketplaces
Find Static thrust and vectoring performance of a spherical convergent flap nozzle with a nonrectangular divergent duct at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.