Explore: Vortex Flaps
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AI-Generated Overview About “vortex-flaps”:
Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
1Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane
By Jay M. Brandon
“Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane” Metadata:
- Title: ➤ Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane
- Author: Jay M. Brandon
- Language: English
- Number of Pages: Median: 35
- Publisher: ➤ For sale by the National Technical Information Service] - National Aeronautics and Space Administration, Scientific and Technical Information Office - Langley Research Center
- Publish Date: 1987
- Publish Location: ➤ [Washington, D.C.] - [Springfield, Va - Hampton, Va
“Piloted-simulation study of effects of vortex flaps on low-speed handling qualities of a delta-wing airplane” Subjects and Themes:
- Subjects: Delta wing airplanes - Vortex flaps - F-106B aircraft - Controllability - Flight simulation
Edition Identifiers:
- The Open Library ID: OL16371484M - OL19247524M - OL18029139M - OL15275200M
Access and General Info:
- First Year Published: 1987
- 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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2Vortex flow aerodynamics, volume I
By James F. Campbell
“Vortex flow aerodynamics, volume I” Metadata:
- Title: ➤ Vortex flow aerodynamics, volume I
- Author: James F. Campbell
- Number of Pages: Median: 395
- Publisher: Langley Research Center
- Publish Date: 1986
- Publish Location: Hampton, Va
“Vortex flow aerodynamics, volume I” Subjects and Themes:
- Subjects: Aerodynamics - Vortex flaps - Vortices
Edition Identifiers:
- The Open Library ID: OL20982435M
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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3Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms
By Kevin J. Kjerstad
“Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms” Metadata:
- Title: ➤ Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms
- Author: Kevin J. Kjerstad
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration, Langley Research Center - Available from NASA Center for AeroSpace Information - National Technical Information Service [distributor
- Publish Date: 1999
- Publish Location: ➤ Springfield, VA - Hanover, MD - Hampton, Va
“Investigation of vortex flaps and other flow control devices on generic high-speed civil transport planforms” Subjects and Themes:
- Subjects: ➤ Vortex flaps - High speed - Planforms - Subsonic wind tunnels - Computational fluid dynamics - Control surfaces - Civil aviation
Edition Identifiers:
- The Open Library ID: OL15569332M
- Online Computer Library Center (OCLC) ID: 44440801
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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4Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m 60 deg delta wing
By K. Rinoie
“Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m 60 deg delta wing” Metadata:
- Title: ➤ Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m 60 deg delta wing
- Author: K. Rinoie
- Number of Pages: Median: 25
- Publisher: ➤ Cranfield Institute of Technology, College of Aeronautics
- Publish Date: 1991
- Publish Location: Cranfield, Bedford, England
“Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m 60 deg delta wing” Subjects and Themes:
- Subjects: Vortex flaps - Vortex plates - Vortices
Edition Identifiers:
- The Open Library ID: OL21379320M
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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5Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing
By Kenichi Rinoie
“Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing” Metadata:
- Title: ➤ Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing
- Author: Kenichi Rinoie
- Number of Pages: Median: 16
- Publisher: National Aerospace Laboratory
- Publish Date: 1992
- Publish Location: Tokyo
“Experimental studies of vortex flaps and vortex plates. Part 1. 0.53m span 60 deg delta wing” Subjects and Themes:
- Subjects: Vortex flaps - Delta wings - Vortex plates
Edition Identifiers:
- The Open Library ID: OL19249019M
Access and General Info:
- First Year Published: 1992
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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6Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap
By Neal T. Frink
“Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap” Metadata:
- Title: ➤ Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap
- Author: Neal T. Frink
- Number of Pages: Median: 309
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Subsonic wind-tunnel measurements of a slender wind-body configuration employing a vortex flap” Subjects and Themes:
- Subjects: Subsonic wind tunnels - Vortex flaps - Vortices
Edition Identifiers:
- The Open Library ID: OL19002817M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
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7The behaviour and performance of leading edge vortex flaps
By D. G. Ellis
“The behaviour and performance of leading edge vortex flaps” Metadata:
- Title: ➤ The behaviour and performance of leading edge vortex flaps
- Author: D. G. Ellis
- Publisher: ➤ College of Aeronautics, Cranfield Institute of Technology
- Publish Date: 1986
- Publish Location: Cranfield, U.K
“The behaviour and performance of leading edge vortex flaps” Subjects and Themes:
- Subjects: Vortex flaps - Leading edge flaps
Edition Identifiers:
- The Open Library ID: OL19987133M
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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8Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps
By Yip. Long P,.
“Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” Metadata:
- Title: ➤ Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps
- Author: Yip. Long P,.
- Number of Pages: Median: 44
- Publisher: Langley Research Center
- Publish Date: 1987
- Publish Location: Hampton, Va
“Wind-tunnel free-flight investigation of a 0.15-scale model of the F-106B airplane with vortex flaps” Subjects and Themes:
- Subjects: Vortex flaps - Free flight - Dynamic stability
Edition Identifiers:
- The Open Library ID: OL19000734M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
Online Marketplaces
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Vortex generator
effectiveness of wings and control surfaces, such as flaps, elevators, ailerons, and rudders. Vortex generators are most often used to delay flow separation
High-lift device
Flaps are usually located on the trailing edge of a wing, while leading edge flaps are used occasionally. There are many kinds of trailing-edge flap.
Vortex lift
behaviour and performance of leading-edge Vortex flaps" (PDF). Retrieved 2023-12-17. "Leading Edge Vortex Allows Bats to Stay Aloft, Aerospace Professor
Gurney flap
to the wing without the flaps. Storms, B. L.; Jang, C. S. (1994). "Lift Enhancement of an Airfoil Using a Gurney Flap and Vortex Generators". Journal of
Blown flap
Blown flaps, blown wing or jet flaps are powered aerodynamic high-lift devices used on the wings of certain aircraft to improve their low-speed flight
Flap (aeronautics)
trailing edges of a fixed-wing aircraft. Flaps are used to reduce the take-off distance and the landing distance. Flaps also cause an increase in drag so they
Wingtip vortices
configuration of the flaps could be changed on existing aircraft to break the vortex into three smaller and less disturbing vortexes. This primarily involved
Insect flight
Stollery, J. L. (1988). "The Behaviour and Performance of Leading-Edge Vortex Flaps" (PDF). ICAS 1988 Jerusalem. 1988. International Council of Aeronautical
Krueger flap
Krueger flaps, or Krüger flaps, are lift enhancement devices that may be fitted to the leading edge of an aircraft wing. Unlike slats or droop flaps, the
Leading-edge slat
and trailing-edge ailerons (i.e. what would later be called trailing-edge flaps) that could be deployed in conjunction with the leading-edge slats to test