Design and Characteristics of a Small Hypersonic Shock Tunnel Combustion Driver PDF Download
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Author: R. E. Duffy
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 0
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Book Description
A combustion driver for a small Hypersonic Shock Tunnel has been designed and tested. Combustion pressure-time histories for stoichiometric hydrogen and oxygen mixtures diluted with varying percentages of helium have been obtained. Tests indicate that the combustion results are repeatable and peak combustion pressure and temperature are controllable within a wide range. The dimensions of combustion drivers appear to have an important effect in that rough burning conditions, reported by other investigators, have not been noticeable except at very low percentage concentrations of helium.
Author: R. E. Duffy
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 0
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Book Description
A combustion driver for a small Hypersonic Shock Tunnel has been designed and tested. Combustion pressure-time histories for stoichiometric hydrogen and oxygen mixtures diluted with varying percentages of helium have been obtained. Tests indicate that the combustion results are repeatable and peak combustion pressure and temperature are controllable within a wide range. The dimensions of combustion drivers appear to have an important effect in that rough burning conditions, reported by other investigators, have not been noticeable except at very low percentage concentrations of helium.
Author: Henry T. Nagamatsu
Publisher:
ISBN:
Category : Hypersonic wind tunnels
Languages : en
Pages : 30
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Book Description
Design features of the General Electric Research Laboratory hypersonic shock tunnel are described. Particular emphasis is placed on many of its unique features. The loading and ignition system for consistent driver combustion without detonation is discussed. The anchoring of the driver and the slip joint clamping section that holds the main scored diaphragm is described in some detail. By boring and honing the stainless steel tubes, the attenuation of the shock wave in the long driven section was minimized. The use of a second diaphragm and a slip joint at the entrance to a conical nozzle is explained. The development of instrumentation necessary for shock tunnel operation is shown to have progressed to a point where the hypersonic shock tunnel is an extremely useful and versatile tool for hypersonic research. It is possible to simulate the Mach numbers and temperatures encountered by ICBM's, satellites, and space vehicles at the high altitude conditions. (Author).
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 1170
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Book Description
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 986
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Book Description
Author: Max E. Wilkins
Publisher:
ISBN:
Category : Helium
Languages : en
Pages : 40
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Book Description
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1318
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Book Description
Author: Michael Peter Wood
Publisher:
ISBN:
Category :
Languages : en
Pages :
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Book Description
Author: Zonglin Jiang
Publisher: Cambridge University Press
ISBN: 1009035673
Category : Technology & Engineering
Languages : en
Pages : 316
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Book Description
Introducing the state-of-the-art of hypervelocity shock tunnels, this complete reference features a variety of drivers and step-by-step introductions to their theories, physics, methods and testing. This book enables researchers and engineers in aerospace to design and improve wind tunnels that simulate flow qualities of real hypersonic flyers.
Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 860
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Book Description
Author: United States. Department of Commerce. Office of Technical Services
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 990
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Book Description
