Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body PDF Download

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Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body

Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body PDF Author: John R. Sevier
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44

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Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body

Aerodynamic Characteristics at Mach Numbers of 1.41 and 2.01 of a Series of Cranked Wings Ranging in Aspect Ratio from 4.00 to 1.74 in Combination with a Body PDF Author: John R. Sevier
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 44

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Book Description

Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94

Aerodynamic Characteristics of Several Cranked Leading-edge Wing-body Combinations at Mach Numbers from 0.4 to 2.94 PDF Author: Edward J. Hopkins
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 98

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Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing

Longitudinal Aerodynamic Characteristics at Mach Number 2.02 of a Series of Wing-body Configurations Employing a Cambered and Twisted Arrow Wing PDF Author: Harry W. Carlson
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Aerodynamic Characteristics in Pitch of Several M-wing-body Combinations at Mach Numbers of 2.40, 2.60, and 2.86

Aerodynamic Characteristics in Pitch of Several M-wing-body Combinations at Mach Numbers of 2.40, 2.60, and 2.86 PDF Author: Odell A. Morris
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 42

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Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground

Aerodynamic Characteristics of Low-aspect-ratio Wings in Close Proximity to the Ground PDF Author: Marvin P. Fink
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2

Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 PDF Author: Lowell E. Hasel
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36

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The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50°

The Aerodynamic Characteristics of Several Thick Delta Wings at Mach Numbers to 6 and Angles of Attack 50° PDF Author: John B. McDevitt
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 114

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A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Two Trapezoidal and Three Delta Wings Having Different Surface Shapes

A Tabulation of Wind-tunnel Pressure Data and Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Two Trapezoidal and Three Delta Wings Having Different Surface Shapes PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 76

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The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93

The Longitudinal Aerodynamic Characteristics of a Sweptback Wing-body Combination with and Without End Plates at Mach Numbers from 0.40 to 0.93 PDF Author: W. P. Henderson
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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A Tabulation of Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Four Swept Wings Having the Same Planform But Different Surface Shapes

A Tabulation of Section Aerodynamic Characteristics at Mach Numbers of 1.61 and 2.01 for Four Swept Wings Having the Same Planform But Different Surface Shapes PDF Author: Emma Jean Landrum
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40

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Book Description