Tabulation of Coordinates for Hypersonic Axisymmetric Nozzles PDF Download
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 126
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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 126
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Book Description
Author: Robert J. Cresci
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 74
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Author: Robert J. Cresci
Publisher:
ISBN:
Category :
Languages : en
Pages : 61
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Book Description
Author: Robert J. Cresci
Publisher:
ISBN:
Category :
Languages : en
Pages : 126
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Book Description
Author: Robert J. Cresci
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 0
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Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 890
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Book Description
Author: Zonglin Jiang
Publisher: Cambridge University Press
ISBN: 131651675X
Category : Technology & Engineering
Languages : en
Pages : 315
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Book Description
A comprehensive reference on the basics, physics, design methods, and testing of various state-of-the art hypervelocity shock tunnels.
Author: Paul Czysz
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 116
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Book Description
The High Temperature Gas Dynamics Facility was developed as a result of the Aeronautical Systems Division's effort to extend the state-of the-art in hypersonic aerodynamic simulation. The facility is a hypersonic wind tunnel supplied with high pressure air, heated from a zirconia dioxide pebble heater. The maximum stagnation pressure and temperature is 40 atres and 4700 R, respectively. This facility is one of four of its kind in this hemisphere and the only Air Force facility of its type. This report discusses the modification of the facility to a two foot diameter test section with a Mach number range of 6 through 14 and its expected performance. This facility is scheduled to be operational in the Fall of 1963.
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 142
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Book Description
Author: John Benjamin Anders
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 52
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