Explore: Wind Tunnel Nozzles
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
By P. S. Barna
“Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” Metadata:
- Title: ➤ Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel
- Author: P. S. Barna
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1995 - 1996
- Publish Location: Hampton, Va - [Springfield, Va
“Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel” Subjects and Themes:
- Subjects: ➤ Acoustic ducts - Blowing - Diffusers - Flow visualization - Nozzle design - Pressure recovery - Scale models - Sound detecting and ranging - Sound waves - Three dimensional models - Velocity measurement - Wind tunnel models - Wind tunnel nozzles - Wind tunnels
Edition Identifiers:
- The Open Library ID: OL17838013M - OL15504898M - OL15504897M - OL17838014M
- Online Computer Library Center (OCLC) ID: 40132872 - 40122403
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.
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2Supersonic quiet-tunnel development for laminar-turbulent transition research
By Steven P. Schneider
“Supersonic quiet-tunnel development for laminar-turbulent transition research” Metadata:
- Title: ➤ Supersonic quiet-tunnel development for laminar-turbulent transition research
- Author: Steven P. Schneider
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1995
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Supersonic quiet-tunnel development for laminar-turbulent transition research” Subjects and Themes:
- Subjects: ➤ Boundary layer equations - Boundary layer transition - Flow characteristics - Flow measurement - Nozzle walls - Supersonic wind tunnels - Wall flow - Wind tunnel nozzles - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL18082383M - OL15415636M - OL17791329M
- Online Computer Library Center (OCLC) ID: 33200505
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.
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3Supersonic laminar flow control research
By Ching F. Lo
“Supersonic laminar flow control research” Metadata:
- Title: ➤ Supersonic laminar flow control research
- Author: Ching F. Lo
- Language: English
- Publisher: ➤ Ames Research Center - National Aeronautics and Space Administration - University of Tennessee, Space Institute - National Technical Information Service, distributor
- Publish Date: 1995 - 1996
- Publish Location: ➤ Tullahoma, TN - [Springfield, Va - Moffett Field, CA - [Washington, DC - Springfield, Va
“Supersonic laminar flow control research” Subjects and Themes:
- Subjects: ➤ Boundary layer stability - Supersonic boundary layers - Boundary layer control - Supersonic flow - Laminar flow - Active control - Computational fluid dynamics - Control systems design - Boundary layer flow - Laminar boundary layer - Boundary layer transition - Wind tunnel nozzles - Stability - Temperature distribution - Wind tunnel tests - Laminar boundary - Wall temperature - Supersonic wind tunnels - Prediction analysis techniques - Nozzle design
Edition Identifiers:
- The Open Library ID: OL15543412M - OL15424662M - OL15506457M
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.
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4Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel
By A. K. Sreekanth
“Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel” Metadata:
- Title: ➤ Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel
- Author: A. K. Sreekanth
- Number of Pages: Median: 25
- Publisher: ➤ Institute of Aerophysics - Dept. of Aeronautical Engineering and Aerophysics
- Publish Date: 1956
- Publish Location: [Downsview, Ont.]
“Performance of a Mach 4 axially symmetric nozzle designed to operate at 40 microns hg. in the UTIA low density wind tunnel” Subjects and Themes:
- Subjects: Low density wind tunnels - Wind tunnel nozzles
Edition Identifiers:
- The Open Library ID: OL18999688M - OL19003973M
Access and General Info:
- First Year Published: 1956
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5Design of a new contraction for the ARL low speed wind tunnel (U)
By J. H. Watmuff
“Design of a new contraction for the ARL low speed wind tunnel (U)” Metadata:
- Title: ➤ Design of a new contraction for the ARL low speed wind tunnel (U)
- Author: J. H. Watmuff
- Number of Pages: Median: 21
- Publisher: ➤ Aeronautical Research Laboratories
- Publish Date: 1986
- Publish Location: Melbourne, Australia
“Design of a new contraction for the ARL low speed wind tunnel (U)” Subjects and Themes:
- Subjects: Subsonic wind tunnels - Wind tunnel nozzles
Edition Identifiers:
- The Open Library ID: OL18926815M
Access and General Info:
- First Year Published: 1986
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle
By Scott C. Asbury
“Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle” Metadata:
- Title: ➤ Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle
- Author: Scott C. Asbury
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1999
- Publish Location: Hampton, Va - Springfield, VA
“Effects of convoluted divergent flap contouring on the performance of a fixed-geometry nonaxisymmetric exhaust nozzle” Subjects and Themes:
- Subjects: ➤ Wind tunnel nozzles - Oblique shock waves - Flow visualization - Boundary layer separation - Nozzle flow - Wind tunnel tests - Convergent-divergent nozzles
Edition Identifiers:
- The Open Library ID: OL15548828M
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.
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7Study of ice accretion on icing wind tunnel components
By James E. Newton
“Study of ice accretion on icing wind tunnel components” Metadata:
- Title: ➤ Study of ice accretion on icing wind tunnel components
- Author: James E. Newton
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Lewis Research Center
- Publish Date: 1986
- Publish Location: [Cleveland, Ohio
“Study of ice accretion on icing wind tunnel components” Subjects and Themes:
- Subjects: ➤ Drop size - Fan blades - Heat exchangers - Ice formation - Icing (Meteorology) - Wind tunnel apparatus - Wind tunnel drives - Wind tunnel nozzles - Wind tunnel tests - Wind tunnels - Wind vanes
Edition Identifiers:
- The Open Library ID: OL16151290M
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 Study of ice accretion on icing wind tunnel components at online marketplaces:
- Amazon: Audiable, Kindle and printed editions.
- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Wind tunnel
A wind tunnel is "an apparatus for producing a controlled stream of air for conducting aerodynamic experiments". The experiment is conducted in the test
Trisonic Wind Tunnel
A Trisonic Wind Tunnel (TWT) is a wind tunnel so named because it is capable of testing in three speed regimes – subsonic, transonic, and supersonic. The
List of wind tunnels
This is an alphabetical list of wind tunnels. "A2 wind tunnel". Retrieved 26 January 2024. "ACE Climatic Wind Tunnel". Retrieved 26 January 2024. "Fly
Supersonic wind tunnel
A supersonic wind tunnel is a wind tunnel that produces supersonic speeds (1.2<M<5) The Mach number and flow are determined by the nozzle geometry. The
Hypersonic wind tunnel
arrangements, dryer, convergent/divergent nozzle, test section, second throat and diffuser. A blow-down wind tunnel has a low vacuum reservoir at the back
Compressible flow
the boundary layer to supersonic shock waves, supersonic wind tunnels, and supersonic nozzle design. Theodore von Kármán, a student of Prandtl, continued
European Transonic Wind Tunnel
transonic wind tunnel (ETW) is a high-Reynolds-number transonic wind tunnel using nitrogen as the test gas. It is one of the world's largest cryogenic wind tunnels
WindShear
Windshear Full Scale Rolling Road Wind Tunnel is an automotive wind tunnel in Concord, North Carolina. In January 2008 Wind Shear, a division of US machine
Windcatcher
A windcatcher, wind tower, or wind scoop (Persian: بادگیر) is a traditional architectural element used to create cross ventilation and passive cooling
MARHy Wind Tunnel
The MARHy Hypersonic low density Wind Tunnel, located at the ICARE Laboratory in Orléans, France, is a research facility used extensively for fundamental