Author: Mohamed Gad-el-Hak
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 92
Book Description
Development of a Device for Controlling the Leading Edge Vortices Ona Delta Wing
Author: Mohamed Gad-el-Hak
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 92
Book Description
Publisher:
ISBN:
Category : Delta wing airplanes
Languages : en
Pages : 92
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 702
Book Description
Flow Field Over the Wing of a Delta-wing Fighter Model with Vortex Control Devices at Mach 0.6 to 1.2
Author: E. Ann Bare
Publisher:
ISBN:
Category :
Languages : en
Pages : 146
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 146
Book Description
NASA Technical Memorandum
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 136
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 136
Book Description
37th AIAA Aerospace Sciences Meeting and Exhibit
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 740
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 740
Book Description
Aeronautical Engineering
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 538
Book Description
Control of Leading-edge Vortices with Suction
Author: Ismet Gursul
Publisher:
ISBN:
Category : Leading edges (Aerodynamics)
Languages : en
Pages : 60
Book Description
Several control techniques have been applied in order to control leading-edge vortices at high angle of attack. The purpose of these control techniques is to influence the strength and structure of the vortices, to generate rolling moment, and to delay vortex breakdown. Since the vorticity of the leading-edge vortices originates from the separation point along the leading-edge, control of development of the shear layer has been chosen as a control strategy in several investigations: blowing and suction in the tangential direction along a rounded leading-edge.
Publisher:
ISBN:
Category : Leading edges (Aerodynamics)
Languages : en
Pages : 60
Book Description
Several control techniques have been applied in order to control leading-edge vortices at high angle of attack. The purpose of these control techniques is to influence the strength and structure of the vortices, to generate rolling moment, and to delay vortex breakdown. Since the vorticity of the leading-edge vortices originates from the separation point along the leading-edge, control of development of the shear layer has been chosen as a control strategy in several investigations: blowing and suction in the tangential direction along a rounded leading-edge.
Government Reports Annual Index
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1262
Book Description
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1262
Book Description
Government Reports Annual Index: Keyword A-L
Author:
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1260
Book Description
Publisher:
ISBN:
Category : Government reports announcements & index
Languages : en
Pages : 1260
Book Description
Government Reports Announcements & Index
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 650
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 650
Book Description