The Aerodynamic Characteristics of a Body in the Flow Field Near the Tip of a Circular-arc Wing of Rectangular Plan Form at a Mach Number of 2.01 PDF Download

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The Aerodynamic Characteristics of a Body in the Flow Field Near the Tip of a Circular-arc Wing of Rectangular Plan Form at a Mach Number of 2.01

The Aerodynamic Characteristics of a Body in the Flow Field Near the Tip of a Circular-arc Wing of Rectangular Plan Form at a Mach Number of 2.01 PDF Author: John P. Gapcynski
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44

Book Description

The Aerodynamic Characteristics of a Body in the Flow Field Near the Tip of a Circular-arc Wing of Rectangular Plan Form at a Mach Number of 2.01

The Aerodynamic Characteristics of a Body in the Flow Field Near the Tip of a Circular-arc Wing of Rectangular Plan Form at a Mach Number of 2.01 PDF Author: John P. Gapcynski
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44

Book Description

The Aerodynamic Characteristics of a Body in the Two-dimensional Flow Field of a Circular-arc Wing at a Mach Number of 2.01

The Aerodynamic Characteristics of a Body in the Two-dimensional Flow Field of a Circular-arc Wing at a Mach Number of 2.01 PDF Author: John P. Gapcynski
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 49

Book Description
A pressure-distribution investigation was conducted in the Langley 4- by 4-foot supersonic pressure tunnel to determine the aerodynamic characteristics of a body with a fineness ratio of 8 in the two-dimensional flow field of an 8 1/3-percent-thick circular-arc wing of rectangular plan form. Data were obtained for several wing-body positions at a Mach number of 2.01 and a Reynolds number of 3,400,000 per foot.

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

Book Description

Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87

Effects of Wing Planform on the Aerodynamic Characteristics of a Wing-body-tail Model at Mach Numbers 1.57, 2.16, and 2.87 PDF Author: Royce L. McKinney
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 52

Book Description

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

Book Description

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

Book Description

Aerodynamic Characteristics at Mach Number 2.01 of an Airplane Configuration Having a Cambered and Twisted Arrow Wing Designed for a Mach Number of 3.0

Aerodynamic Characteristics at Mach Number 2.01 of an Airplane Configuration Having a Cambered and Twisted Arrow Wing Designed for a Mach Number of 3.0 PDF Author: Odell A. Morris
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 38

Book Description

Aerodynamic Characteristics in Pitch of Several Ring-wing-body Configurations at a Mach Number of 2.2

Aerodynamic Characteristics in Pitch of Several Ring-wing-body Configurations at a Mach Number of 2.2 PDF Author: Odell A. Morris
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 26

Book Description

Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63

Longitudinal Aerodynamic Characteristics of Several High-drag Bodies at Mach Numbers from 1.50 to 4.63 PDF Author: James F. Campbell
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44

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

Book Description

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