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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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 : 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

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

Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45© Swept-wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail

Investigation of the Aerodynamic Characteristics in Pitch and Sideslip of a 45© Swept-wing Airplane Configuration with Various Vertical Locations of the Wing and Horizontal Tail PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34

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Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the effects of wing and horizontal-tail vertical location on the aerodynamic characteristics in sideslip at various angles of attack for a supersonic airplane configuration at Mach numbers of 1.41 and 2.01. The basic model was equipped with a wing and horizontal tail, each having 45 degree sweep and an aspect ratio of 4. The wing had a taper ratio of 0.2 and NACA 65A004 sections; the horizontal tail had a taper ratio of 0.4 and NACA 65A006 sections.

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

Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75°

Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75° PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38

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Book Description

Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-wing- Sweep V/STOL Configurations with Outboard Wing Panels Swept Back 75 Deg

Aerodynamic Characteristics in Pitch at a Mach Number of 1.97 of Two Variable-wing- Sweep V/STOL Configurations with Outboard Wing Panels Swept Back 75 Deg PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

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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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Book Description

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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Book Description