Hypersonic Shock-heated Flow Parameters for Velocities to 46,000 Feet Per Second and Altitudes to 323,000 Feet

Hypersonic Shock-heated Flow Parameters for Velocities to 46,000 Feet Per Second and Altitudes to 323,000 Feet PDF Author: Paul William Huber
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 88

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Hypersonic Shock-heated Flow Parameters for Velocities to 46,000 Feet Per Second and Altitudes to 323,000 Feet

Hypersonic Shock-heated Flow Parameters for Velocities to 46,000 Feet Per Second and Altitudes to 323,000 Feet PDF Author: Paul William Huber
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 88

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Hypersonic Shock-heated Flow Parameters for Velocities to 46,000 Feet Per Second and Altitudes to 323,000 Feet [with List of References]

Hypersonic Shock-heated Flow Parameters for Velocities to 46,000 Feet Per Second and Altitudes to 323,000 Feet [with List of References] PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 74

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Hypersonic shook-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet

Hypersonic shook-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet PDF Author: Paul William Huber
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages :

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NASA Technical Report

NASA Technical Report PDF Author:
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 722

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A Flight Measurement of Optical Radiation from Shock-heated Air by Using a Trailblazer II Vehicle

A Flight Measurement of Optical Radiation from Shock-heated Air by Using a Trailblazer II Vehicle PDF Author: Lloyd S. Keafer
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 40

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 666

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Hypersonic and High Temperature Gas Dynamics

Hypersonic and High Temperature Gas Dynamics PDF Author: John David Anderson
Publisher: AIAA
ISBN: 9781563474590
Category : Science
Languages : en
Pages : 710

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Book Description
This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.

Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50,000 Per Second (15.24 Kilometers Per Second)

Charts for Equilibrium Isentropic Expansion of Air Behind Shocks Up to 50,000 Per Second (15.24 Kilometers Per Second) PDF Author: Ernest V. Zoby
Publisher:
ISBN:
Category : Air
Languages : en
Pages : 58

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Charts of Equilibrium Real-gas Stagnation Point Conditions on a Sphere for Altitudes to 200,000 Feet and Velocities to 15,000 Feet Per Second

Charts of Equilibrium Real-gas Stagnation Point Conditions on a Sphere for Altitudes to 200,000 Feet and Velocities to 15,000 Feet Per Second PDF Author: P. D. Fisher
Publisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 60

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Book Description
This report presents in graphical form the stagnation point pressure, temperature, equilibrium surface temperature, and heating rate for a sphere. Equilibrium real-gas effects and surface radiation are considered. The charts cover a range of velocities from 0 to 15,000 feet per second and altitudes from sea level to 200,000 feet. Corrections for sphere diameter and emissivity are included. (Author).

NASA Technical Note

NASA Technical Note PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 416

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