Explore: Oscillating Wing Aerodynamics
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Books Results
Source: The Open Library
The Open Library Search Results
Search results from The Open Library
12-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
By R. A. Piziali
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Metadata:
- Title: ➤ 2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall
- Author: R. A. Piziali
- Language: English
- Number of Pages: Median: 559
- Publisher: ➤ National Technical Information Service, distributor - Ames Research Center - National Aeronautics and Space Administration, Ames Research Center : US Army Aviation and Troop Command
- Publish Date: 1994
- Publish Location: ➤ Moffett Field, Calif - Moffett Field, Ca - [Springfield, Va
“2-D and 3-D oscillating wing aerodynamics for a range of angles of attack including stall” Subjects and Themes:
- Subjects: ➤ Rotary wings - Aerodynamic coefficients - Pressure distribution - Wind tunnel tests - Wind oscillations - Angle of attack - Airfoils - Aerodynamic stalling - Semispan models - Stalling - Oscillating wing aerodynamics
Edition Identifiers:
- The Open Library ID: OL17007551M - OL15409387M - OL18079048M - OL19754822M - OL17114716M
- Online Computer Library Center (OCLC) ID: 32770651
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.
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2Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations
By James D. Fairgrieve
“Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations” Metadata:
- Title: ➤ Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations
- Author: James D. Fairgrieve
- Publisher: ➤ Dept. of Aerospace Science and Engineering - Institute for Aerospace Studies
- Publish Date: 1979 - 1982
- Publish Location: [Downsview, Ont.]
“Propulsive performance of two dimensional thin airfoils undergoing large amplitude pitch and plunge oscillations” Subjects and Themes:
- Subjects: Oscillating wing aerodynamics - Propulsion - Flapping wing - Unsteady aerodynamics - Airfoils
Edition Identifiers:
- The Open Library ID: OL20968307M - OL19988546M
Access and General Info:
- First Year Published: 1979
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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3Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing
By Jiro Nakamichi
“Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing” Metadata:
- Title: ➤ Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing
- Author: Jiro Nakamichi
- Number of Pages: Median: 23
- Publisher: National Aerospace Laboratory
- Publish Date: 1988
- Publish Location: Tokyo
“Some computations of unsteady Navier-Stokes flow around oscillating airfoil/wing” Subjects and Themes:
- Subjects: Oscillating wing aerodynamics - Unsteady flow - Navier-Stokes equation
Edition Identifiers:
- The Open Library ID: OL19379707M
Access and General Info:
- First Year Published: 1988
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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4Oscillating behaviour of a 7.5% circular arc airfoil
By David James Ahier
“Oscillating behaviour of a 7.5% circular arc airfoil” Metadata:
- Title: ➤ Oscillating behaviour of a 7.5% circular arc airfoil
- Author: David James Ahier
- Publisher: ➤ Dept. of Aerospace Science and Engineering
- Publish Date: 1987
- Publish Location: [Downsview, Ont.]
“Oscillating behaviour of a 7.5% circular arc airfoil” Subjects and Themes:
- Subjects: Oscillating wing aerodynamics - Lift
Edition Identifiers:
- The Open Library ID: OL19000044M
Access and General Info:
- First Year Published: 1987
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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Wiki
Source: Wikipedia
Wikipedia Results
Search Results from Wikipedia
Stall (fluid dynamics)
fixed-wing aircraft. The principles of stall discussed here translate to foils in other fluids as well. A stall is a condition in aerodynamics and aviation
Oscillation
example, the phenomenon of flutter in aerodynamics occurs when an arbitrarily small displacement of an aircraft wing (from its equilibrium) results in an
Lift (force)
"The Aerodynamics of Sail Interaction" (PDF). Archived from the original (PDF) on July 7, 2011. Retrieved July 12, 2011. One explanation of how a wing .
Aeroelasticity
Aeroelasticity problems can be prevented by adjusting the mass, stiffness or aerodynamics of structures which can be determined and verified through the use of
Fixed-wing aircraft
from rotary-wing aircraft (in which a rotor mounted on a spinning shaft generates lift), and ornithopters (in which the wings oscillate to generate lift)
Insect flight
attached directly to the wings. In other winged insects, flight muscles attach to the thorax, which make it oscillate in order to induce the wings to beat
Ornithopter
D. DeLaurier, "An Overview of Micro Air Vehicle Aerodynamics", Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications, Paul Zarchan
Kármán vortex street
Ratio of inertial to viscous forces acting on a liquid Vortex shedding – Oscillating flow effect resulting from fluid passing over a blunt body Vortex-induced
Vortex
Effect in physics Strouhal number – Dimensionless number describing oscillating flow mechanisms Vortex engine – Alternative to tall chimneys Vortex tube –
Tailplane
rotates around the centre of gravity. For example, when the aircraft is oscillating, but is momentarily aligned with the overall vehicle's motion, the tailplane