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

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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

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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

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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

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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

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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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Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3

Force, Moment, and Flow-field Characteristics of Two Wing-body-nacelle Combinations at Mach Numbers 2 and 3 PDF Author: Hill, Jr. (William A.)
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 102

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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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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 :
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Pages : 20

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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 :
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Pages : 34

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Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap

Aerodynamic Characteristics at Mach Number 4.04 of a Rectangular Wing of Aspect Ratio 1.33 Having a 6-percent-thick Circular-arc Profile and a 30-percent-chord Full-span Trailing-edge Flap PDF Author: Robert W. Dunning
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Book Description