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Investigating Aerodynamic Forces on a Delta Wing with Partial Leading Edge Blowing

Investigating Aerodynamic Forces on a Delta Wing with Partial Leading Edge Blowing PDF Author:
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Languages : en
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Investigating Aerodynamic Forces on a Delta Wing with Partial Leading Edge Blowing

Investigating Aerodynamic Forces on a Delta Wing with Partial Leading Edge Blowing PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Prediction of Unsteady Aerodynamics and Control of Delta Wings with Tangential Leading Edge Blowing

Prediction of Unsteady Aerodynamics and Control of Delta Wings with Tangential Leading Edge Blowing PDF Author: Stanford University. Department of Aeronautics and Astronautics
Publisher:
ISBN:
Category :
Languages : en
Pages : 396

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Exploratory Investigation of the Effects of Blowing from the Leading Edge of a Delta Wing

Exploratory Investigation of the Effects of Blowing from the Leading Edge of a Delta Wing PDF Author: W. J. G. Trebble
Publisher:
ISBN:
Category :
Languages : en
Pages : 19

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A Theoretical and Computational Study on the Effects of Leading Edge Lateral Blowing on Delta Wing Aerodynamics

A Theoretical and Computational Study on the Effects of Leading Edge Lateral Blowing on Delta Wing Aerodynamics PDF Author: John S. Hong
Publisher:
ISBN:
Category :
Languages : en
Pages : 288

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An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels

An Investigation at Subsonic Speeds of the Longitudinal Aerodynamic Characteristics at Angles of Attach from -4° to 100° of Delta-wing Reentry Configurations Having Vertically Displaced and Cambered Wing-tip Panels PDF Author: Bernard Spencer
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 40

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Book Description
Subsonic aerodynamic characteristics of delta-wing reentry vehicle with vertically displaced and cambered wing-tip panels.

Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section

Aerodynamic Characteristics of a Delta Wing with Leading Edge Swept Back 45 Degrees, Aspect Ratio 4, and NACA 65A006 Airfoil Section PDF Author: William C. Sleeman
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 34

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This paper presents the results of the investigation of wing-alone and wing-fuselage combination employing a delta wing having 45 degree sweepback of the leading edge, aspect ratio 4, and an NACA 65A006 airfoil section. Lift, drag, pitching moment, and root bending moment were obtained for these configurations. In addition, effective downwash angles and dynamic-pressure characteristics in the region of a probable tail location also were obtained for these configurations, and are presented for a range of tail heights at one tail length. In order to expedite publishing of these data, only a brief analysis is included.

A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0

A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 PDF Author: Robert S. Osborne
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20

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The Lift of Sharp-leading-edged Delta Wings with Blowing

The Lift of Sharp-leading-edged Delta Wings with Blowing PDF Author: Joint Institute for Aeronautics and Acoustics. Joint Institute for Aeronautics and Acoustics
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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Controlled Vortical Flow on Delta Wings Through Unsteady Leading Edge Blowing

Controlled Vortical Flow on Delta Wings Through Unsteady Leading Edge Blowing PDF Author: K. T. Lee
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 178

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Influence of Airfoil Geometry on Delta Wing Leading-edge Vortices and Vortex-induced Aerodynamics at Supersonic Speeds

Influence of Airfoil Geometry on Delta Wing Leading-edge Vortices and Vortex-induced Aerodynamics at Supersonic Speeds PDF Author: Richard M. Wood
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 88

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