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Shock Tubes

Shock Tubes
Author: Irving Israel Glass
Publisher: University of Toronto Press
Total Pages: 852
Release: 1970-12-15
Genre: Education
ISBN: 1487597584

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This volume contains the proceedings of a symposium held at the University of Toronto in June 1969. The symposium consisted of six sessions; each containing an invited paper, followed by six contributed papers reporting on recent, relevant research and development. The topics are: a review of research problems in basic shock tube flows and the possibilities for the shock tube in the future; driving techniques; explosive drivers; theoretical and experimental research in electromagnetic shock tubes; chemical kinetics and spectroscopy; and a review of shock tube diagnostics, instrumentation and fundamental data as well as the measurement of physical quantities.


Shock Tubes and Waves

Shock Tubes and Waves
Author: Charles E. Treanor
Publisher: SUNY Press
Total Pages: 1130
Release: 1982-01-01
Genre: Philosophy
ISBN: 9780873955959

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Proceedings from a symposium on shock tubes and waves held July 6-9, 1981.


Shock Tubes

Shock Tubes
Author: I. I. Glass
Publisher: [Toronto, Ont.] : University of Toronto Press
Total Pages: 860
Release: 1970
Genre: Shock tubes
ISBN:

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Shock Tubes

Shock Tubes
Author: John Keith Wright
Publisher:
Total Pages: 188
Release: 1961
Genre: Shock tubes
ISBN:

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Shock Waves and Shock Tubes

Shock Waves and Shock Tubes
Author: International Symposium on Shock Waves and Shock tubes (Berkeley, Calif.))
Publisher:
Total Pages: 915
Release: 1986
Genre:
ISBN:

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A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification

A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification
Author: Robert L. Trimpi
Publisher:
Total Pages: 674
Release: 1955
Genre: Gas flow
ISBN:

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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.