Author: H. Clyde McLemore
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 57
Book Description
An investigation has been conducted in the Langley full-scale tunnel to determine the effects on the low-speed aerodynamic characteristics of blowing air over the trailing-edge flap of a large-scale wing-body-tail model. The wing and horizontal tail have an aspect ratio of 3.5, taper ratio of 0.3, leading-edge sweep of 49 degrees, and NACA 65A006 airfoil sections parallel to the plane of symmetry. The trailing-edge air was ejected over highly deflected half- and full-span flaps in combination with several leading-edge-flow control devices including blowing from a slot in the wing leading edge. The momentum coefficient range was investigated was 0 to 0.16 for the trailing-edge blowing and 0 to 0.025 for the leading-edge blowing. Most of the tests were conducted at a Reynolds number of 5,200,000 corresponding to a Mach number of 0.08.
Blowing Over the Flaps and Wing Leading Edge of a Thin 49 Degree Swept Wing-body-tail Configuration in Combination with Leading-edge Devices
Author: H. Clyde McLemore
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 57
Book Description
An investigation has been conducted in the Langley full-scale tunnel to determine the effects on the low-speed aerodynamic characteristics of blowing air over the trailing-edge flap of a large-scale wing-body-tail model. The wing and horizontal tail have an aspect ratio of 3.5, taper ratio of 0.3, leading-edge sweep of 49 degrees, and NACA 65A006 airfoil sections parallel to the plane of symmetry. The trailing-edge air was ejected over highly deflected half- and full-span flaps in combination with several leading-edge-flow control devices including blowing from a slot in the wing leading edge. The momentum coefficient range was investigated was 0 to 0.16 for the trailing-edge blowing and 0 to 0.025 for the leading-edge blowing. Most of the tests were conducted at a Reynolds number of 5,200,000 corresponding to a Mach number of 0.08.
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 57
Book Description
An investigation has been conducted in the Langley full-scale tunnel to determine the effects on the low-speed aerodynamic characteristics of blowing air over the trailing-edge flap of a large-scale wing-body-tail model. The wing and horizontal tail have an aspect ratio of 3.5, taper ratio of 0.3, leading-edge sweep of 49 degrees, and NACA 65A006 airfoil sections parallel to the plane of symmetry. The trailing-edge air was ejected over highly deflected half- and full-span flaps in combination with several leading-edge-flow control devices including blowing from a slot in the wing leading edge. The momentum coefficient range was investigated was 0 to 0.16 for the trailing-edge blowing and 0 to 0.025 for the leading-edge blowing. Most of the tests were conducted at a Reynolds number of 5,200,000 corresponding to a Mach number of 0.08.
High-pressure Blowing Over Flap and Wing Leading Edge of a Large-scale 49 Degrees Swept Wing-body-tail Configuration in Combination with a Drooped Nose and a Nose with a Radius Increase
Author: Marvin P. Fink
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
High-pressure Blowing Over Flap and Wing Leading Edge of a Thin Large-scale 49 Degree Swept Wing-body-tail Configuration in Combination with a Drooped Nose and a Nose with a Radius Increase
Author: Marvin P. Fink
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 40
Book Description
A 49 degree swept-wing complete model equipped for high-pressure blowing full span at two chordwise locations at the leading edge of a full-span wing and over a half-span flap has been tested in the Langley full-scale tunnel to determine the effectiveness of blowing at the leading edge as a supplementary leading-edge stall control at high lift coefficients.
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 40
Book Description
A 49 degree swept-wing complete model equipped for high-pressure blowing full span at two chordwise locations at the leading edge of a full-span wing and over a half-span flap has been tested in the Langley full-scale tunnel to determine the effectiveness of blowing at the leading edge as a supplementary leading-edge stall control at high lift coefficients.
High-pressure Blowing Over Flap and Wing Leading Edge of a Thin Large-scale 49° Swept Wing-body-tail Configuration in Combination with a Drooped Nose and a Nose with a Radius Increase
Author: Marvin P. Fink
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 40
Book Description
Research Abstracts and Reclassification Notice
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category :
Languages : en
Pages : 496
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 496
Book Description
Surface Pressure Distributions on a Large-scale 49© Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge
Author: H. Clyde McLemore
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 134
Book Description
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 134
Book Description
Aerodynamic Characteristics in Sideslip of a Large-scale 49 Degree Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge
Author: H. Clyde McLemore
Publisher:
ISBN:
Category :
Languages : en
Pages : 46
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 46
Book Description
Surface Pressure Distributions on a Large-scale 49 Degree Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge
Author: H. Clyde McLemore
Publisher:
ISBN:
Category :
Languages : en
Pages : 128
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 128
Book Description
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1370
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Aerodynamic Characteristics of a Large-Scale Unswept Wing-Body-Tail Configuration with Blowing Applied Over the Flap and Wind Leading Edge
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 228
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 228
Book Description