Explore: Turbulent Wakes
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes
By Osama A. Kandil
“Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes” Metadata:
- Title: ➤ Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes
- Author: Osama A. Kandil
- Language: English
- Publisher: ➤ [National Aeronautics and Space Administration - National Technical Information Service, distributor - American Institute of Aeronautics and Astronautics
- Publish Date: 1996
- Publish Location: ➤ Washington, DC - Springfield, Va
“Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Shear stress - Vortices - Turbulent wakes - Finite difference theory - Supersonic transports - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL17593620M - OL15508580M - OL17132483M - OL18122329M
- Online Computer Library Center (OCLC) ID: 41899956
Access and General Info:
- First Year Published: 1996
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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2Prediction and control of vortex-dominated and vortex-wake flows
By Osama Kandil
“Prediction and control of vortex-dominated and vortex-wake flows” Metadata:
- Title: ➤ Prediction and control of vortex-dominated and vortex-wake flows
- Author: Osama Kandil
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Old Dominion University Research Foundation - National Aeronautics and Space Administration
- Publish Date: 1993 - 1996
- Publish Location: ➤ Springfield, Va - [Washington, DC - Norfolk, Va
“Prediction and control of vortex-dominated and vortex-wake flows” Subjects and Themes:
- Subjects: ➤ Turbulent flow - Vortex-motion - Aircraft wakes - Turbulent wakes - Vortices - Predictions - Active control
Edition Identifiers:
- The Open Library ID: OL15481466M - OL14706547M
Access and General Info:
- First Year Published: 1993
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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3Direct numerical simulation of a temporally evolving incompressible plane wake
By R. Sondergaard
“Direct numerical simulation of a temporally evolving incompressible plane wake” Metadata:
- Title: ➤ Direct numerical simulation of a temporally evolving incompressible plane wake
- Author: R. Sondergaard
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - Joint Institute for Aeronautics and Acoustics - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1997
- Publish Location: ➤ [Moffett Field, Calif.] - Stanford, CA - [Springfield, Va
“Direct numerical simulation of a temporally evolving incompressible plane wake” Subjects and Themes:
- Subjects: Computational fluid dynamics - Fast Fourier transformations - Incompressible flow - Navier-Stokes equation - Turbulent wakes
Edition Identifiers:
- The Open Library ID: OL15479109M
Access and General Info:
- First Year Published: 1997
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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4Second order modeling of boundary-free turbulent shear flows
By Tsan-Hsing Shih
“Second order modeling of boundary-free turbulent shear flows” Metadata:
- Title: ➤ Second order modeling of boundary-free turbulent shear flows
- Author: Tsan-Hsing Shih
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - NASA Lewis Research Center, Institute for Computational Mechanics in Propulsion
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Cleveland, Ohio
“Second order modeling of boundary-free turbulent shear flows” Subjects and Themes:
- Subjects: ➤ Jet flow - Mixing layers (Fluids) - Reynolds stress - Shear flow - Shear layers - Turbulent flow - Turbulent wakes - Vortices
Edition Identifiers:
- The Open Library ID: OL15399181M
Access and General Info:
- First Year Published: 1991
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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5The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction
By William J. Devenport
“The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction” Metadata:
- Title: ➤ The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction
- Author: William J. Devenport
- Language: English
- Publisher: ➤ Dept. of Aerospace and Ocean Engineering, Virginia Polytechnic Institute and State University - National Technical Information Service, distributor - National Aeronautics and Space Administration
- Publish Date: 1997
- Publish Location: ➤ Springfield, Va - [Washington, DC - Blacksburg, VA
“The spectral and statistical properties of turbulence generated by a vortex/blade-tip interaction” Subjects and Themes:
- Subjects: ➤ Helicopters - Rotary wings - Aeroacoustics - Blade tips - Blade slap noise - Statistical distributions - Noise prediction - Blade-vortex interaction - Aerodynamic noise - Turbulent wakes - Interactional aerodynamics - Incompressible flow
Edition Identifiers:
- The Open Library ID: OL15479176M
Access and General Info:
- First Year Published: 1997
- 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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6Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails
By Robert W. Moses
“Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails” Metadata:
- Title: ➤ Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails
- Author: Robert W. Moses
- Language: English
- Publisher: ➤ American Institute of Aeronautics and Astronautics - National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1998
- Publish Location: ➤ Springfield, Va - [Washington, DC - Reston, Va
“Spatial characteristics of the unsteady differential pressures on 16% F/A-18 vertical tails” Subjects and Themes:
- Subjects: ➤ F-18 aircraft - Vortices - Angle of attack - Buffeting - Leading edges - Aerodynamic forces - Turbulent wakes - Aeroelasticity
Edition Identifiers:
- The Open Library ID: OL15509422M
Access and General Info:
- First Year Published: 1998
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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7Computational aerodynamics of ordered vortex flows
By H. W. M. Hoeijmakers
“Computational aerodynamics of ordered vortex flows” Metadata:
- Title: ➤ Computational aerodynamics of ordered vortex flows
- Author: H. W. M. Hoeijmakers
- Number of Pages: Median: 195
- Publisher: National Aerospace Laboratory
- Publish Date: 1989
- Publish Location: Amsterdam
“Computational aerodynamics of ordered vortex flows” Subjects and Themes:
- Subjects: Turbulent wakes - Vortex sheets - Vortices
Edition Identifiers:
- The Open Library ID: OL21039416M
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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8Radar reflectivity in wingtip-generated wake vortices
By Marshall, Robert E.
“Radar reflectivity in wingtip-generated wake vortices” Metadata:
- Title: ➤ Radar reflectivity in wingtip-generated wake vortices
- Author: Marshall, Robert E.
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: Hampton, Va - Springfield, VA
“Radar reflectivity in wingtip-generated wake vortices” Subjects and Themes:
- Subjects: ➤ Airports - Commercial aircraft - Detection - Turbulent wakes - Vortices - Wakes
Edition Identifiers:
- The Open Library ID: OL15547175M
Access and General Info:
- First Year Published: 1997
- 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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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Wake turbulence
produce wake turbulence. Helicopter wakes may be significantly stronger than those of a fixed-wing aircraft of the same weight. The strongest wake will occur
Turbulence
In fluid dynamics, turbulence or turbulent flow is fluid motion characterized by chaotic changes in pressure and flow velocity. It is in contrast to laminar
Reynolds number
laminar (sheet-like) flow, while at high Reynolds numbers, flows tend to be turbulent. The turbulence results from differences in the fluid's speed and direction
Wake (physics)
free surface and gravity (or surface tension). The wake is the region of disturbed flow (often turbulent) downstream of a solid body moving through a fluid
Coherent turbulent structure
There were also early correlation data found by measuring jets and turbulent wakes, particularly by Corrsin and Roshko. Hama's hydrogen bubble technique
Golf ball
on the upstream side of the ball to transition from laminar to turbulent. The turbulent boundary layer is able to remain attached to the surface of the
Drag coefficient
causing the wake to be narrow. A high form drag results in a broad wake. The boundary layer will transition from laminar to turbulent if Reynolds number
Computational fluid dynamics
confinement (VC) method is an Eulerian technique used in the simulation of turbulent wakes. It uses a solitary-wave like approach to produce a stable solution
John Gibson (actor, born 1948)
says captain of the business jet might not have realized he was in the turbulent wake of a 757". Los Angeles Times. p. 3. Retrieved 2024-02-27. John Gibson
Magnus effect
studies show that a turbulent wake behind the spinning ball causes aerodynamic drag, plus there is a noticeable angular deflection in the wake, and this deflection