Explore: Inlet Nozzles
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Source: The Open Library
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Search results from The Open Library
1Shock-tunnel combustor testing for hypersonic vehicles
By Mark Loomis
“Shock-tunnel combustor testing for hypersonic vehicles” Metadata:
- Title: ➤ Shock-tunnel combustor testing for hypersonic vehicles
- Author: Mark Loomis
- Language: English
- Publisher: ➤ MCAT Institute - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ Springfield, Va - San Jose, Calif - [Washington, DC
“Shock-tunnel combustor testing for hypersonic vehicles” Subjects and Themes:
- Subjects: ➤ Wind tunnel tests - Two dimensional flow - Hypersonic flow - Supersonic combustion ramjet engines - Propulsion system performance - Propulsion system configurations - Engine tests - Air breathing engines - Hypersonic speed - Combustion chambers - Hypersonic aircraft - Hypersonic inlets - Inlet nozzles - Mach number
Edition Identifiers:
- The Open Library ID: OL17001315M - OL18076085M - OL15403346M
- Online Computer Library Center (OCLC) ID: 32198098
Access and General Info:
- First Year Published: 1994
- 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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2An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications
By Paul L. McDill
“An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications” Metadata:
- Title: ➤ An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications
- Author: Paul L. McDill
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1986
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va
“An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications” Subjects and Themes:
- Subjects: Ducts - Turboprop engines - Inlet nozzles - Diffusers - Gears
Edition Identifiers:
- The Open Library ID: OL15407512M
Access and General Info:
- First Year Published: 1986
- 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 An experimental evaluation of S-duct inlet-diffuser configurations for turboprop offset gearbox applications at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.