Surface Pressure Distributions on a Large-scale 49 Degree Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge

Surface Pressure Distributions on a Large-scale 49 Degree Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge PDF Author: H. Clyde McLemore
Publisher:
ISBN:
Category :
Languages : en
Pages : 128

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Surface Pressure Distributions on a Large-scale 49© Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge

Surface Pressure Distributions on a Large-scale 49© Sweptback Wing-body-tail Configuration with Blowing Applied Over the Flaps and Wing Leading Edge PDF Author: H. Clyde McLemore
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 134

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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

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 PDF Author: H. Clyde McLemore
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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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

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 PDF Author: Marvin P. Fink
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

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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

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 PDF Author: Marvin P. Fink
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 40

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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

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 PDF Author: Marvin P. Fink
Publisher:
ISBN:
Category : Air flow
Languages : en
Pages : 40

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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.

Aerodynamic Characteristics of a Large-Scale Unswept Wing-Body-Tail Configuration with Blowing Applied Over the Flap and Wind Leading Edge

Aerodynamic Characteristics of a Large-Scale Unswept Wing-Body-Tail Configuration with Blowing Applied Over the Flap and Wind Leading Edge PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 228

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Aerodynamic Characteristics and Pressure Distributions of a 6 Percent-thick 49 Degree Sweptback Wing with Blowing Over Half-span and Full-span Flaps

Aerodynamic Characteristics and Pressure Distributions of a 6 Percent-thick 49 Degree Sweptback Wing with Blowing Over Half-span and Full-span Flaps PDF Author: Edward F. Jr Whittle
Publisher:
ISBN:
Category :
Languages : en
Pages : 71

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Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61

Pressure Distributions and Aerodynamic Characteristics of Several Spoiler Controls on a 40 Degree Sweptback Wing at a Mach Number of 1.61 PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 70

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Investigation at Large Scale of the Pressure Distribution and Flow Phenomena Over a Wing with the Leading Edge Swept Back 47.5 Degrees Having Circular-arc Airfoil Sections and Equipped with Drooped-nose and Plain Flaps

Investigation at Large Scale of the Pressure Distribution and Flow Phenomena Over a Wing with the Leading Edge Swept Back 47.5 Degrees Having Circular-arc Airfoil Sections and Equipped with Drooped-nose and Plain Flaps PDF Author: Roy H. Lange
Publisher:
ISBN:
Category :
Languages : en
Pages : 72

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