A Study of Real Gas Phenomena Related to Shock Tube Performance PDF Download
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Author: Rolf P. Andersen
Publisher:
ISBN:
Category : Gases at high temperatures
Languages : en
Pages : 106
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Book Description
Author: Rolf P. Andersen
Publisher:
ISBN:
Category : Gases at high temperatures
Languages : en
Pages : 106
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Book Description
Author: N. Muniswamy Reddy
Publisher:
ISBN:
Category : Measurement
Languages : en
Pages : 28
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Book Description
Shock tube flow analysis with dimensionless velocity number.
Author: Theodore A. Brabbs
Publisher:
ISBN:
Category : Gas dynamics
Languages : en
Pages : 20
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Book Description
Author: Harold Vincent Wright
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 262
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Book Description
Author: Shao Chi Lin
Publisher:
ISBN:
Category : Aerothermodynamics
Languages : en
Pages : 18
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Book Description
In recent years, a considerable volume of research was undertaken in the ield f high temperature gas dynamics in which the shock tube was employed as the principal experimental tool. In particular, a substantial fraction of this research effort was devoted to the study of phenomena peculiar to air and its component gases, and is, therefore, directly applicable to many aerophysics problems associated with hypersonic flight through the Earth's atmosphere. However, in spite of their omniexistence, most of these works were published over a period of time in a scattered manner, and hence, appear to be somewhat incoherent. A preliminary effort is made to compile these published works under various identifiable (if somewhat arbitrary) topics so as to provide a more convenient reference for investigators in this field. Whenever possible, the advantages and limitations of the shock tube as a research tool for tackling the various topics of interest are also pointed out. (Author).
Author: Robert L. Trimpi
Publisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 674
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Book Description
The nonlinear characteristic differential equations applicable to a quasi-one-dimensional unsteady channel flow with friction and heat transfer are linearized and integrated in functional form for the particular study of small perturbations from ideal shock-tube flows. If the equivalence of unsteady- and steady-flow boundary layers is assumed, the problem of determining the perturbation in the unsteady flow reduces to an evaluation of the drag of a flat plate in the equivalent steady flow.
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: 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: Alfred Gordon Gaydon
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 344
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Book Description
Author: Aeronautical Research Council
Publisher:
ISBN:
Category :
Languages : en
Pages : 0
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