Explore: Supersonic Diffusers
Discover books, insights, and more — all in one place.
Learn more about Supersonic Diffusers with top reads curated from trusted sources — all in one place.
AI-Generated Overview About “supersonic-diffusers”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application
By Kamlesh Kapoor
“A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application” Metadata:
- Title: ➤ A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application
- Author: Kamlesh Kapoor
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1994
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Bypasses - Flow distortion - Civil aviation - Cross flow - Inlet flow - Diffusers - Navier-Stokes equation - Mass flow - Supersonic inlets - Supersonic diffusers - Supersonic transports
Edition Identifiers:
- The Open Library ID: OL17114056M - OL17002076M - OL18076587M - OL15404445M
- Online Computer Library Center (OCLC) ID: 32309713
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 A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
2Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
“Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: Masashi Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Inviscid flow - Supersonic diffusers - Computational grids - Two dimensional flow - Turbulence models - Navier-Stokes equation - Supersonic inlets
Edition Identifiers:
- The Open Library ID: OL15414474M - OL17116401M - OL18081585M
Access and General Info:
- First Year Published: 1995
- 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 Parametrics on 2D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
33D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By M. Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: M. Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL17117540M - OL17106503M
- Online Computer Library Center (OCLC) ID: 35282961
Access and General Info:
- First Year Published: 1995
- 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 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
4Factors affecting the performance of supersonic diffusers
By A. M. Patterson
“Factors affecting the performance of supersonic diffusers” Metadata:
- Title: ➤ Factors affecting the performance of supersonic diffusers
- Author: A. M. Patterson
- Number of Pages: Median: 22
- Publisher: ➤ [Institute of Aerophysics] - Institute of Aerophysics
- Publish Date: 1952
- Publish Location: [Downsview, Ont.]
“Factors affecting the performance of supersonic diffusers” Subjects and Themes:
- Subjects: Supersonic diffusers
Edition Identifiers:
- The Open Library ID: OL20897534M - OL19986958M
Access and General Info:
- First Year Published: 1952
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Factors affecting the performance of supersonic diffusers at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
53D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
By Masashi Mizukami
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Metadata:
- Title: ➤ 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet
- Author: Masashi Mizukami
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Springfield, Va - [Washington, DC]
“3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet” Subjects and Themes:
- Subjects: ➤ Computational fluid dynamics - Boundary layers - Supersonic diffusers - Computational grids - Boundary layer separation - Turbulence models - Three dimensional flow - Flow distribution - Engine inlets - Internal flow - Leading edges - Shock wave interaction - Navier-Stokes equation - Shock waves
Edition Identifiers:
- The Open Library ID: OL18086923M - OL15423278M
Access and General Info:
- First Year Published: 1995
- 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 3D Navier-Stokes analysis of a Mach 2.68 bifurcated rectangular mixed-compression inlet at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
6Further tests with a variable ramp intake having a design Mach number of 2.2
By M. C. Neale
“Further tests with a variable ramp intake having a design Mach number of 2.2” Metadata:
- Title: ➤ Further tests with a variable ramp intake having a design Mach number of 2.2
- Author: M. C. Neale
- Language: English
- Publisher: H.M.S.O.
- Publish Date: 1966
- Publish Location: London
“Further tests with a variable ramp intake having a design Mach number of 2.2” Subjects and Themes:
- Subjects: Supersonic diffusers
Edition Identifiers:
- The Open Library ID: OL6016955M
- Online Computer Library Center (OCLC) ID: 6157431
- Library of Congress Control Number (LCCN): 66075050
Access and General Info:
- First Year Published: 1966
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Further tests with a variable ramp intake having a design Mach number of 2.2 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
7Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41
By John M. Smith
“Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Metadata:
- Title: ➤ Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41
- Author: John M. Smith
- Language: English
- Number of Pages: Median: 37
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: Washington - Springfield, Va
“Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Subjects and Themes:
- Subjects: Airplanes - Combustion - Supersonic diffusers - Turbojet engines
Edition Identifiers:
- The Open Library ID: OL17818391M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
8Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41
By John M Smith
“Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Metadata:
- Title: ➤ Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41
- Author: John M Smith
- Language: English
- Number of Pages: Median: 37
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - Washington
“Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Subjects and Themes:
- Subjects: Airplanes - Combustion - Turbojet engines - Supersonic diffusers
Edition Identifiers:
- The Open Library ID: OL14932011M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
9Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41
By John M. Smith
“Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Metadata:
- Title: ➤ Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41
- Author: John M. Smith
- Language: English
- Number of Pages: Median: 37
- Publisher: ➤ for sale by the National Technical Information Service - National Aeronautics and Space Administration, Scientific and Technical Information Office
- Publish Date: 1978
- Publish Location: Springfield, Va - Washington
“Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41” Subjects and Themes:
- Subjects: Airplanes - Combustion - Turbojet engines - Supersonic diffusers
Edition Identifiers:
- The Open Library ID: OL17647705M
Access and General Info:
- First Year Published: 1978
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Performance of a short annular dump diffuser using suction-stabilized vortices at inlet Mach numbers to 0.41 at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
10Supersonic diffusors for large pressure recovery
By Kenneth C. Livingston
“Supersonic diffusors for large pressure recovery” Metadata:
- Title: ➤ Supersonic diffusors for large pressure recovery
- Author: Kenneth C. Livingston
- Number of Pages: Median: 88
- Publisher: ➤ Dept. of Aeronautical Engineering, University of Toronto
- Publish Date: 1948
- Publish Location: Toronto
“Supersonic diffusors for large pressure recovery” Subjects and Themes:
- Subjects: Supersonic diffusers
Edition Identifiers:
- The Open Library ID: OL20985032M
Access and General Info:
- First Year Published: 1948
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Supersonic diffusors for large pressure recovery at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
11Supersonic inlets
By Ione D. V. Faro
“Supersonic inlets” Metadata:
- Title: Supersonic inlets
- Author: Ione D. V. Faro
- Language: English
- Number of Pages: Median: 158
- Publisher: ➤ North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development
- Publish Date: 1965
- Publish Location: [Paris]
“Supersonic inlets” Subjects and Themes:
- Subjects: Air intakes - Airplanes - Jet propulsion - Supersonic diffusers
Edition Identifiers:
- The Open Library ID: OL5531016M
- Online Computer Library Center (OCLC) ID: 1838021
- Library of Congress Control Number (LCCN): 67006377
Access and General Info:
- First Year Published: 1965
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
Find Supersonic inlets at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Diffuser (thermodynamics)
important role in a supersonic diffuser. Diffusers are very common in heating, ventilating, and air-conditioning systems. Diffusers are used in both all-air
Compressible flow
aircraft inlet design, objects in supersonic flight, and (at a more fundamental level) supersonic nozzles and diffusers. Depending on the flow conditions
Ramjet
engine to provide air for combustion. Ramjets work most efficiently at supersonic speeds around Mach 3 (2,300 mph; 3,700 km/h) and can operate up to Mach 6
Inlet cone
(sometimes called shock cones or inlet centerbodies) are a component of some supersonic aircraft and missiles. They are primarily used on ramjets, such as the
Scramjet
A scramjet (supersonic combustion ramjet) is a variant of a ramjet airbreathing jet engine in which combustion takes place in supersonic airflow. As in
Arthur Kantrowitz
propulsion were published in 1988. His early research included supersonic diffusers and supersonic compressors in the early 40s, which has since been applied
Diffuser
Look up diffuser or diffusers in Wiktionary, the free dictionary. Diffuser may refer to: Diffuser (automotive), a shaped section of a car's underbody
Unstart
In supersonic aerodynamics, an unstart refers to a generally violent breakdown of the supersonic airflow. The phenomenon occurs when mass flow rate changes
Nozzle
distribution of air via ceiling diffusers is not possible or not practical. Diffusers that uses jet nozzles are called jet diffuser where it will be arranged
Kantrowitz limit
Arthur; duP, Coleman (May 1945). "Preliminary Investigation of Supersonic Diffusers" (PDF). Advance Confidential Report L5D20. Archived (PDF) from the