Explore: Wing Tips
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
By Lawrence C. Freudinger
“Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods” Metadata:
- Title: ➤ Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods
- Author: Lawrence C. Freudinger
- Language: English
- Number of Pages: Median: 18
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division
- Publish Date: 1989
- Publish Location: ➤ [Washington, D.C.] - [Springfield, VA
“Flutter clearance of the F-18 high-angle-of-attack research vehicle with experimental wingtip instrumentation pods” Subjects and Themes:
- Subjects: ➤ Vibration - Flutter (Aerodynamics) - Hornet (Jet fighter plane) - Research aircraft - F-18 aircraft - Wing tips - Angle of attack - Clearances - Flutter
Edition Identifiers:
- The Open Library ID: OL17630290M - OL16139104M
- Online Computer Library Center (OCLC) ID: 24899921
Access and General Info:
- First Year Published: 1989
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Access
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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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2Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
By Osama A. Kandil
“Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” Metadata:
- Title: ➤ Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications
- Author: Osama A. Kandil
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - Dept. of Aerospace Engineering, College of Engineering & Technology, Old Dominion University - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Washington, DC - Norfolk, Va - Springfield, Va
“Aeroelastic, CFD, and dynamics computation and optimization for buffet and flutter applications” Subjects and Themes:
- Subjects: ➤ Aeroelasticity - Buffeting - Computational fluid dynamics - Delta wings - Flutter - Vortices - Wing tips
Edition Identifiers:
- The Open Library ID: OL17593616M - OL15508543M
- Online Computer Library Center (OCLC) ID: 40618623
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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3Turbulence measurements in the near field of a wingtip vortex
By Jim Chow
“Turbulence measurements in the near field of a wingtip vortex” Metadata:
- Title: ➤ Turbulence measurements in the near field of a wingtip vortex
- Author: Jim Chow
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Ames Research Center - National Technical Information Service, distributor
- Publish Date: 1997
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Turbulence measurements in the near field of a wingtip vortex” Subjects and Themes:
- Subjects: ➤ Stress tensors - Turbulent flow - Flow measurement - Vortices - Near fields - Wing tips - Reynolds stress - Wind tunnel tests
Edition Identifiers:
- The Open Library ID: OL15498161M - OL17834421M
- Online Computer Library Center (OCLC) ID: 39705632
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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4NACA 0015 wing pressure and trailing vortex measurements
By Kenneth W. McAlister
“NACA 0015 wing pressure and trailing vortex measurements” Metadata:
- Title: ➤ NACA 0015 wing pressure and trailing vortex measurements
- Author: Kenneth W. McAlister
- Language: English
- Publisher: ➤ National Technical Information Service , distributor] - National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program
- Publish Date: 1991
- Publish Location: ➤ [Springfield, Va - Washington, D.C
“NACA 0015 wing pressure and trailing vortex measurements” Subjects and Themes:
- Subjects: ➤ Vortices - Pressure measurement - Wing tips - Velocity measurement - Trailing edges - Low speed - Semispan models - Wings
Edition Identifiers:
- The Open Library ID: OL17725370M
Access and General Info:
- First Year Published: 1991
- 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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5Further developments of the fringe-imaging skin friction technique
By Gregory G. Zilliac
“Further developments of the fringe-imaging skin friction technique” Metadata:
- Title: ➤ Further developments of the fringe-imaging skin friction technique
- Author: Gregory G. Zilliac
- Language: English
- Publisher: ➤ National Technical Information Service, distributor - National Aeronautics and Space Administration, Ames Research Center
- Publish Date: 1996
- Publish Location: ➤ [Springfield, Va - Moffett Field, Calif
“Further developments of the fringe-imaging skin friction technique” Subjects and Themes:
- Subjects: ➤ Skin friction - Flow distribution - Diffraction patterns - Three dimensional flow - Wing tips - Imaging techniques - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL15542045M
Access and General Info:
- First Year Published: 1996
- 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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6Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex
By Brooks A. Childers
“Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex” Metadata:
- Title: ➤ Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex
- Author: Brooks A. Childers
- Language: English
- Number of Pages: Median: 22
- Publisher: ➤ For sale by the National Technical Information Service - National Aeronautics and Space Administration, Langley Research Center
- Publish Date: 1990
- Publish Location: Hampton, Va - [Springfield, Va
“Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex” Subjects and Themes:
- Subjects: ➤ Photographs - Vortex-motion - Vortices - Cameras - Wing tips - Image analysis - Smoke - Measurement - Flight tests
Edition Identifiers:
- The Open Library ID: OL16131052M
Access and General Info:
- First Year Published: 1990
- 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 Video photographic considerations for measuring the proximity of a probe aircraft with a smoke seeded trailing vortex at online marketplaces:
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- Ebay: New & used books.
Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Wing tip
A wing tip (or wingtip) is the part of the wing that is most distant from the fuselage of a fixed-wing aircraft. Because the wing tip shape influences
Wingtip device
intended to improve the efficiency of fixed-wing aircraft by reducing drag. Although there are several types of wing tip devices which function in different manners
Wing configuration
Ju 87 Stuka dive bomber. Cranked or canted tip: tip section dihedral differs from the main wing. The tips may have upwards dihedral as on the F-4 Phantom
Brogue shoe
The brogue (from Scottish Gaelic bròg and Irish Gaelic bróg, both meaning "shoe") is a style of low-heeled shoe or boot traditionally characterised by
Forward-swept wing
the wing tips to such an extent that the tips stall first and one of the main characteristics of the design is lost, on a conventional wing the tips always
Stall (fluid dynamics)
stalls before the tip. However, when taken beyond stalling incidence the tips may still become fully stalled before the inner wing despite initial separation
Wingtip vortices
left behind a wing as it generates lift. The name is a misnomer because the cores of the vortices are slightly inboard of the wing tips. Wingtip vortices
Lift (force)
three-dimensional wing involves significant additional issues, especially relating to the wing tips. For a wing of low aspect ratio, such as a typical delta wing, two-dimensional
Closed wing
closed wing is a wing that effectively has two main planes that merge at their ends so that there are no conventional wing tips. Closed wing designs
Delta wing
name "Delta", used a very gentle angle so that the wing appeared almost straight and the wing tips had to be cropped sharply (see below). His first such