Aerodynamic Characteristics of a Truncated-cone Lifting Reentry Body at Mach Numbers from 10 to 21

Aerodynamic Characteristics of a Truncated-cone Lifting Reentry Body at Mach Numbers from 10 to 21
Title Aerodynamic Characteristics of a Truncated-cone Lifting Reentry Body at Mach Numbers from 10 to 21 PDF eBook
Author
Publisher
Pages 44
Release 1963
Genre
ISBN

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NASA Technical Note

NASA Technical Note
Title NASA Technical Note PDF eBook
Author
Publisher
Pages 422
Release 1968
Genre
ISBN

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Proceedings of the ... Army Numerical Analysis Conference

Proceedings of the ... Army Numerical Analysis Conference
Title Proceedings of the ... Army Numerical Analysis Conference PDF eBook
Author
Publisher
Pages 494
Release 1972
Genre Numerical analysis
ISBN

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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
Title 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 eBook
Author Roger H. Fournier
Publisher
Pages 76
Release 1967
Genre Space vehicles
ISBN

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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.

Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300

Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300
Title Aerodynamic Force Characteristics of a Series of Lifting Cone and Cone-cylinder Configurations at a Mach Number of 6.83 and Angles of Attack Up to 1300 PDF eBook
Author Jim A. Penland
Publisher
Pages 50
Release 1961
Genre Mach number
ISBN

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A Computer Program for Systematically Analyzing Free-flight Data to Determine the Aerodynamics of Axisymmetric Bodies

A Computer Program for Systematically Analyzing Free-flight Data to Determine the Aerodynamics of Axisymmetric Bodies
Title A Computer Program for Systematically Analyzing Free-flight Data to Determine the Aerodynamics of Axisymmetric Bodies PDF eBook
Author Gerald N. Malcolm
Publisher
Pages 40
Release 1968
Genre Aerodynamic characteristics
ISBN

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Proceedings

Proceedings
Title Proceedings PDF eBook
Author
Publisher
Pages 256
Release 1972
Genre Computer programs
ISBN

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