The Numerical Solution of the Expulsion of a Shock Wave from the Open End of a Cylindrical Shock Tube

The Numerical Solution of the Expulsion of a Shock Wave from the Open End of a Cylindrical Shock Tube PDF Author: Edward David Spong
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ISBN:
Category :
Languages : en
Pages : 276

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Transactions of the ... Conference of Army Mathematicians

Transactions of the ... Conference of Army Mathematicians PDF Author:
Publisher:
ISBN:
Category : Mathematics
Languages : en
Pages : 624

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Dissertation Abstracts International

Dissertation Abstracts International PDF Author:
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ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 1276

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A Numerical Solution for the Interaction of a Moving Shock Wave with a Turbulent Mixing Region

A Numerical Solution for the Interaction of a Moving Shock Wave with a Turbulent Mixing Region PDF Author: William Fred Walker
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ISBN:
Category : Shock waves
Languages : en
Pages : 216

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Numerical Results for the Diffraction of a Normal Shock Wave by a Sphere and for the Subsequent Transient Flow

Numerical Results for the Diffraction of a Normal Shock Wave by a Sphere and for the Subsequent Transient Flow PDF Author: Richard W. Barnwell
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 44

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The finite-difference method which Peter D. Lax developed for treating unsteady inviscid flow fields is used to study the transient flow in the shock layer of a sphere that has been struck by a normal shock wave. Transient flow of this sort is encountered when a shock tube is used as a supersonic wind tunnel. Time histories of the shock detachment distance and the stagnation-point pressure and tangential velocity gradient are presented for ranges of the incident-shock Mach number and the perfect-gas specific-heat ratio. These results show that the stagnation-point pressure approaches the steady value much more rapidly than the shock detachment distance. In general, the stagnation-point pressure but more rapidly than the shock detachment distance. As the specific-heat ratio is decreased and the incident-shock Mach number is increased, the variation of the velocity gradient with respect to the shock detachment distance becomes more nearly linear.

Preliminary Investigation of the Shock Wave Propagated from the Open End of a Cylindrical Shock Tube

Preliminary Investigation of the Shock Wave Propagated from the Open End of a Cylindrical Shock Tube PDF Author: G. Beichler
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ISBN:
Category : Shock waves
Languages : en
Pages : 18

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National Union Catalog

National Union Catalog PDF Author:
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ISBN:
Category : Union catalogs
Languages : en
Pages : 616

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Includes entries for maps and atlases.

a study of cylidrical shock waves in a sector tube

a study of cylidrical shock waves in a sector tube PDF Author: a. cole
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ISBN:
Category :
Languages : en
Pages : 164

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Comprehensive Dissertation Index, 1861-1972: Engineering: general and aeronautical

Comprehensive Dissertation Index, 1861-1972: Engineering: general and aeronautical PDF Author: Xerox University Microfilms
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ISBN:
Category : Dissertations, Academic
Languages : en
Pages : 906

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A Study of Shock-tube Phenomena

A Study of Shock-tube Phenomena PDF Author: Harold Vincent Wright
Publisher:
ISBN:
Category : Shock waves
Languages : en
Pages : 262

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