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Aerodynamic Characteristics of a Series of Bodies with Variations in Nose Camber

Aerodynamic Characteristics of a Series of Bodies with Variations in Nose Camber PDF Author: Barrett L. Shrout
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 60

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Book Description

Aerodynamic Characteristics of a Series of Bodies with Variations in Nose Camber

Aerodynamic Characteristics of a Series of Bodies with Variations in Nose Camber PDF Author: Barrett L. Shrout
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 60

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Book Description

Aerodynamic Characteristics of a Series of Bodies with Variations in Nose Camber

Aerodynamic Characteristics of a Series of Bodies with Variations in Nose Camber PDF Author: Barrett L. Shrout
Publisher:
ISBN:
Category : Drag (Aerodynamics)
Languages : en
Pages : 60

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Book Description

The Effect of Camber on the Aerodynamic Characteristics of a Body at a Mach Number of 2.01

The Effect of Camber on the Aerodynamic Characteristics of a Body at a Mach Number of 2.01 PDF Author: John P. Gapcynski
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 22

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Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58 Degrees and Mach Numbers to 2

Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58 Degrees and Mach Numbers to 2 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 104

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Book Description

Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 589 and Mach Numbers to 2

Investigation of the Asymmetric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 589 and Mach Numbers to 2 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 96

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Book Description

Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Degrees to 53 Degrees at Mach Numbers from 2.30 to 4.62

Experimental and Theoretical Study of Aerodynamic Characteristics of Some Lifting Bodies at Angles of Attack from -10 Degrees to 53 Degrees at Mach Numbers from 2.30 to 4.62 PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 32

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Investigation of the Assymtric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58 [degrees] and Mach Numbers to 2

Investigation of the Assymtric Aerodynamic Characteristics of Cylindrical Bodies of Revolution with Variations in Nose Geometry and Rotational Orientation at Angles of Attack to 58 [degrees] and Mach Numbers to 2 PDF Author: Robert L. Kruse
Publisher:
ISBN:
Category :
Languages : en
Pages : 93

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 68

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Aerodynamic Characteristics of 2-, 3-, and 4-, Caliber Tangent-ogive Cylinders with Nose Bluffness Ratios of 0.00, 0.25, 0.50, and 0.75 at Mach Numbers from 0.6 to 4.0

Aerodynamic Characteristics of 2-, 3-, and 4-, Caliber Tangent-ogive Cylinders with Nose Bluffness Ratios of 0.00, 0.25, 0.50, and 0.75 at Mach Numbers from 0.6 to 4.0 PDF Author: Carroll B. Butler
Publisher:
ISBN:
Category : Radomes
Languages : en
Pages : 248

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Book Description
This report summarizes wind tunnel test data on various body alone configurations which provide a data matrix for bluff and pointed bodies of revolution with systematic variations in nose bluffness, nose fineness ratio, and cylinder afterbody fineness ratio. Modular model components were used to obtain static stability and drag data, with emphasis on the effect of nose bluffness on drag. Although data is included for tangent ogive noses of fineness ratio 2, 2.25, 2.5, 3.0, and 4, the nose fineness ratios of 2, 3, and 4 calibers include a systematic variation in nose bluffness ratios of 0.00, 0.25, 0.50, and 0.75 on cylindrical midsections of 5, 7, 9, and 11 calibers. A 1-caliber cylindrical afterbody is used with all configurations in this report.

A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0

A Parametric Study of the Aerodynamic Characteristics of Nose-cylinder-flare Bodies at a Mach Number of 6.0 PDF Author: George C. Ashby
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 82

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Book Description