Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 PDF Download

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Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06

Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 PDF Author: Sleeman, Jr. (William C.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 56

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Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06

Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 PDF Author: Sleeman, Jr. (William C.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 56

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Book Description

Aerodynamic Characteristics of a 60 Degree Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06

Aerodynamic Characteristics of a 60 Degree Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 54

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Book Description

Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06

Aerodynamic Characteristics of a 60° Sweptback-wing Airplane Configuration Having Tail Surfaces Located Outboard of the Wingtips at Mach Numbers of 2.30, 2.97, 3.51, and 4.06 PDF Author: Sleeman, Jr. (William C.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 49

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Book Description

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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Investigation of Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, and 3.51

Investigation of Aerodynamic Characteristics of an Airplane Configuration Having Tail Surfaces Outboard of the Wing Tips at Mach Numbers of 2.30, 2.97, and 3.51 PDF Author: James D. Church
Publisher:
ISBN:
Category :
Languages : en
Pages : 48

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Book Description

Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design

Static Longitudinal and Lateral Aerodynamic Characteristics at a Mach Number of 2.20 of a V/STOL Airplane Configuration with a Variable-sweep Wing and with a Skewed Wing Design PDF Author: Odell A. Morris
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32

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Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards

Aerodynamic Characteristics at Mach Numbers of 1.5, 1.8, and 2.0 of a Blended Wing-body Configuration with and Without Integral Canards PDF Author: A. Warner Robins
Publisher:
ISBN:
Category : Hypersonic planes
Languages : en
Pages : 68

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Effects of Wing and Tail Location on the Aerodynamic Characteristics of an Airplane for Mach Numbers from 0.25 to 4.63

Effects of Wing and Tail Location on the Aerodynamic Characteristics of an Airplane for Mach Numbers from 0.25 to 4.63 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 34

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Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable- Sweep Wings

Stability and Control Characteristics at a Mach Number of 1.97 of an Airplane Configuration Having Two Types of Variable- Sweep Wings PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 48

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Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63

Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 3.96 and 4.63 PDF Author: Maurice O. Feryn
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Book Description