Explore: Airfoil Oscillations
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Source: The Open Library
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1Control of unsteady separated flow associated with the dynamic stall of airfoils
By Michael C. Wilder
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Metadata:
- Title: ➤ Control of unsteady separated flow associated with the dynamic stall of airfoils
- Author: Michael C. Wilder
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor - MCAT Institute
- Publish Date: 1992 - 1994 - 1995
- Publish Location: ➤ Springfield, Va - [Washington, DC - Springfield, Va.? - San Jose, CA
“Control of unsteady separated flow associated with the dynamic stall of airfoils” Subjects and Themes:
- Subjects: ➤ Unsteady flow - Wind tunnel tests - Leading edges - Aerodynamic stalling - Boundary layer control - Unsteady flow (Aerodynamics) - Separated flow - Boundary layer separation - Reynolds number - Supercritical airfoils - Airfoil oscillations - Airfoil profiles - Airfoils - Mach number - Active control
Edition Identifiers:
- The Open Library ID: OL15365679M - OL15408283M - OL15415078M
Access and General Info:
- First Year Published: 1992
- 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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2Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
By Euromech Colloquium (349th 1996 Göttingen, Germany)
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Metadata:
- Title: ➤ Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method
- Author: ➤ Euromech Colloquium (349th 1996 Göttingen, Germany)
- Language: English
- Publisher: ➤ National Aeronautics and Space Administration - National Technical Information Service, distributor
- Publish Date: 1996
- Publish Location: ➤ [Washington, DC - Springfield, Va
“Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method” Subjects and Themes:
- Subjects: ➤ Airfoil oscillations - Airfoils - Boundary layer separation - Computational fluid dynamics - Coupling - Mach number - Separated flow - Transonic flow - Transonic flutter - Transonic speed - Unsteady flow - Viscous flow
Edition Identifiers:
- The Open Library ID: OL17595884M - OL15518388M
- Online Computer Library Center (OCLC) ID: 42671384
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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3TULIPS: a method to calculate transonic potential flow about oscillating airfoils
By H. Schippers
“TULIPS: a method to calculate transonic potential flow about oscillating airfoils” Metadata:
- Title: ➤ TULIPS: a method to calculate transonic potential flow about oscillating airfoils
- Author: H. Schippers
- Number of Pages: Median: 36
- Publisher: National Aerospace Laboratory
- Publish Date: 1988
- Publish Location: Amsterdam, Netherlands
“TULIPS: a method to calculate transonic potential flow about oscillating airfoils” Subjects and Themes:
- Subjects: Transonic flow - Airfoil oscillations
Edition Identifiers:
- The Open Library ID: OL21378477M
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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4Investigation of the oscillatory derivatives of an aerofoil with flaps oscillating at negative angles of attack
By G. Kurylowich
“Investigation of the oscillatory derivatives of an aerofoil with flaps oscillating at negative angles of attack” Metadata:
- Title: ➤ Investigation of the oscillatory derivatives of an aerofoil with flaps oscillating at negative angles of attack
- Author: G. Kurylowich
- Number of Pages: Median: 16
- Publisher: Institute of Aerophysics
- Publish Date: 1961
- Publish Location: [Downsview, Ont.]
“Investigation of the oscillatory derivatives of an aerofoil with flaps oscillating at negative angles of attack” Subjects and Themes:
- Subjects: Flutter - Airfoil oscillations
Edition Identifiers:
- The Open Library ID: OL20968660M
Access and General Info:
- First Year Published: 1961
- Is Full Text Available: No
- Is The Book Public: No
- Access Status: No_ebook
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