Explore: Inlet Nozzles
Discover books, insights, and more — all in one place.
Learn more about Inlet Nozzles with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “inlet-nozzles”:
Books Results
Source: The Open Library
The Open Library Search Results
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
Find Shock-tunnel combustor testing for hypersonic vehicles at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
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.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
De Laval nozzle
switched to a converging-diverging nozzle in his steam jet pumps by 1878 after using convergent nozzles but these nozzles remained a company secret. In 1888
Surface effect ship
on by air or sea, and it can use water jets for propulsion since the inlet nozzles are always covered by water. The United States Navy initiated the SES
Components of jet engines
intake (inlet) — For subsonic aircraft, the inlet is a duct which is required to ensure smooth airflow into the engine despite air approaching the inlet from
Compressible flow
applications such as: aircraft inlet design, objects in supersonic flight, and (at a more fundamental level) supersonic nozzles and diffusers. Depending on
Metropolitan-Vickers F.2
combustion chamber, which caused warping and fracturing of the turbine inlet nozzles. Around seven weeks after its first flight, on 4th January 1944, DG204/G
Rocket engine nozzle
Controlled flow-separation nozzles include: expanding nozzle, bell nozzles with a removable insert, stepped nozzles, or dual-bell nozzles. These are generally
Rotodynamic pump
the inlet nozzle (at the suction) is empty or filled with the air it will damage the impeller. The difference between pressure created at the inlet nozzle
Lockheed SR-71 Blackbird
60086 711 8, p. 328. "Variable Area Exhaust Nozzle", U.S. Patent 3,062,003 "Variable Geometry Exhaust Nozzles and Their Effects on Airplane Performance"
Turbofan
Turbofan engine noise propagates both upstream via the inlet and downstream via the primary nozzle and the by-pass duct. Other noise sources are the fan
Combustor
Astronautics. ISBN 1-56347-538-3. Mattingly, Jack D. (2006). "Chapter 10: Inlets, Nozzles, and Combustion Systems". Elements of Propulsion: Gas Turbines and