Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6 PDF Download

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Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6

Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6 PDF Author: Michael F. Sarabia
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6

Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 3 to 6 PDF Author: Michael F. Sarabia
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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Book Description

Aerodynamic Characteristics of a Blunt, Half-cone Entry Configuration, with Horizontal Landing Capability

Aerodynamic Characteristics of a Blunt, Half-cone Entry Configuration, with Horizontal Landing Capability PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4

Aerodynamic Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers of 5.2, 7.4, and 10.4 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 78

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Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 10.9 to 21.2 in Helium

Characteristics of a Blunt Half-cone Entry Configuration at Mach Numbers from 10.9 to 21.2 in Helium PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 96

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The Aerodynamic Characteristics of a Blunt Half Cone Entry Configurations Obtained from Ballistic Range Tests at Mach Numbers Near 3

The Aerodynamic Characteristics of a Blunt Half Cone Entry Configurations Obtained from Ballistic Range Tests at Mach Numbers Near 3 PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 38

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Flow Field and Surface Pressures on a Blunt Half-cone Entry Configuration at Mach Numbers of 7.4 and 10.4

Flow Field and Surface Pressures on a Blunt Half-cone Entry Configuration at Mach Numbers of 7.4 and 10.4 PDF Author: George H. Holdaway
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 62

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Book Description

Aerodynamic Characteristics of Two Blunt, Half-cone Wedge Entry Configurations at Mach Numbers from 2.30 to 4.63

Aerodynamic Characteristics of Two Blunt, Half-cone Wedge Entry Configurations at Mach Numbers from 2.30 to 4.63 PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category :
Languages : en
Pages : 33

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The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90

The Lateral and Directional Aerodynamic Characteristics of a Re-entry Configuration Based on a Blunt 13° Half Cone at Mach Numbers to 0.90 PDF Author: George C. Kenyon
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 54

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NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 616

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Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Variable-geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control

Aerodynamic Characteristics at Mach Numbers from 1.50 to 4.63 of a Variable-geometry Lifting Reentry Concept Employing Elevator and Body Base Flaps for Control PDF Author: Roger H. Fournier
Publisher:
ISBN:
Category : Space vehicles
Languages : en
Pages : 76

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Book Description
An investigation of a lifting body configuration has been conducted in the Langley Unitary Plan wind tunnel through a Mach number range from 1.50 to 4.63 to determine the control effectiveness characteristics of body base flaps with and without anhedral tail elevator controls.