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Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Book Description
The Aerospace Hypersonic Shock Tunnel is described along with an initial calibration at flow Mach numbers of 12, 14, 17, and 18. Room temperature helium is used as the driver gas. Efforts to drive the shock tunnel with com bustion heated helium have been made, and these experiments are also described.
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 20
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Book Description
The Aerospace Hypersonic Shock Tunnel is described along with an initial calibration at flow Mach numbers of 12, 14, 17, and 18. Room temperature helium is used as the driver gas. Efforts to drive the shock tunnel with com bustion heated helium have been made, and these experiments are also described.
Author: Raymond Brun
Publisher: Springer Science & Business Media
ISBN: 3642788297
Category : Science
Languages : en
Pages : 497
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Book Description
Recently, there have been significant advances in the fields of high-enthalpy hypersonic flows, high-temperature gas physics, and chemistry shock propagation in various media, industrial and medical applications of shock waves, and shock-tube technology. This series contains all the papers and lectures of the 19th International Symposium on Shock Waves held in Marseille in 1993. They are published in four topical volumes, each containing papers on related topics, and preceded by an overview written by a leading international expert. The volumes may be purchased independently.
Author: Frank K. Lu
Publisher: AIAA
ISBN: 9781600864483
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 694
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Book Description
Author: Cornell Aeronautical Laboratory
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 46
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Book Description
Author: Cornell Aeronautical Laboratory. Experimental Facilities Division
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 52
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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: R. E. Duffy
Publisher:
ISBN:
Category : Combustion
Languages : en
Pages : 1
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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: Charles E. Wittliff
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 118
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Book Description
Author: Raymond Brun
Publisher: Springer
ISBN: 9783540577102
Category : Science
Languages : en
Pages : 485
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Book Description
Recently, there have been significant advances in the fields of high-enthalpy hypersonic flows, high-temperature gas physics, and chemistry shock propagation in various media, industrial and medical applications of shock waves, and shock-tube technology. This series contains all the papers and lectures of the 19th International Symposium on Shock Waves held in Marseille in 1993. They are published in four topical volumes, each containing papers on related topics, and preceded by an overview written by a leading international expert. The volumes may be purchased independently.
Author: F.R. Riddell
Publisher: Elsevier
ISBN: 0323142621
Category : Transportation
Languages : en
Pages : 769
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Book Description
Progress in Astronautics and Rocketry, Volume 7: Hypersonic Flow Research compiles papers presented at a conference on hypersonics held at the Massachusetts Institute of Technology in August 1961. This book discusses the low Reynolds number effects, chemical kinetics effects, inviscid flow calculations, and experimental techniques relating to the problems in acquiring an understanding of hypersonic flow. The structure and composition of hypersonic wakes with attendant complex chemical kinetic effects is only briefly mentioned. This text consists of five parts. Parts A to C comprise of theoretical papers on the problems of calculating flow fields at hypersonic speeds. The experimental techniques that are of immediate practical interest in view of the difficulty of flight testing are discussed in Parts D and E. This publication is beneficial to engineers involved in advanced design problems.
