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

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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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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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NASA Technical Note

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

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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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Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7

Static Stability and Control Characteristics of a Half-cone Entry Configuration at Mach Numbers from 2.2 to 0.7 PDF Author: Ralph W. Holtzclaw
Publisher:
ISBN:
Category :
Languages : en
Pages : 68

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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.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 978

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Large-scale Wind-tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody

Large-scale Wind-tunnel Investigation of an M1-L Lifting Body with an Inflatable and a Rigid Afterbody PDF Author: Kenneth W. Mort
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 36

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Aerodynamic Characteristics of a Flat-bottom Canted-nose Half-cone Reentry Configuration at a Mach Number of 6.7

Aerodynamic Characteristics of a Flat-bottom Canted-nose Half-cone Reentry Configuration at a Mach Number of 6.7 PDF Author: William O. Armstrong
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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A Preliminary Investigation of Modified Blunt 13° Half-cone Re-entry Configurations at Subsonic Speeds

A Preliminary Investigation of Modified Blunt 13° Half-cone Re-entry Configurations at Subsonic Speeds PDF Author: George C. Kenyon
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 54

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Monthly Catalog of United States Government Publications

Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1388

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