Equations And Charts For Determining The Hypersonic Stability Derivates Of Combinations Of Cone Frustums Computed By Newtonian Impact Theory PDF Download

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NASA Technical Note

NASA Technical Note
Author:
Publisher:
Total Pages: 406
Release: 1960
Genre:
ISBN:

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Applied Mechanics Reviews

Applied Mechanics Reviews
Author:
Publisher:
Total Pages: 1006
Release: 1960
Genre: Mechanics, Applied
ISBN:

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Theoretical Evaluation of Hypersonic Forces, Moments, and Stability Derivatives for Combinations of Flat Plates, Including Effects of Blunt Leading Edges, by Newtonian Impact Theory

Theoretical Evaluation of Hypersonic Forces, Moments, and Stability Derivatives for Combinations of Flat Plates, Including Effects of Blunt Leading Edges, by Newtonian Impact Theory
Author: Walter B. Olstad
Publisher:
Total Pages: 70
Release: 1962
Genre: Aerodynamic load
ISBN:

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Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares

Effects of Afterbody Shape on the Aerodynamic Characteristics of a Fineness-ratio-10 Cone- Cylinder Configuration at Mach Numbers from 1.57 to 4.65 Including Design Parameter Curves for Circular Afterbody Flares
Author: A. B. Carraway
Publisher:
Total Pages: 124
Release: 1960
Genre:
ISBN:

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Stability Derivatives of Cones at Supersonic Speeds

Stability Derivatives of Cones at Supersonic Speeds
Author: Murray Tobak
Publisher:
Total Pages: 43
Release: 1956
Genre: Cones
ISBN:

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The aerodynamic stability derivatives due to pitching velocity and vertical acceleration are derived for circular cones traveling at supersonic speeds. Both first-order and a combination of first and second order potential solutions are obtained, and in calculations for the forces, no approximations are made to the tangency condition or the isentropic pressure relation. In addition, expressions for the forces, moments, and stability derivatives of arbitrary bodies of revolution are derived from Newtonian impact theory.