Uniform Flow Duration in Shock Tubes
Author | : Robert Ples Humphreys |
Publisher | : |
Total Pages | : 90 |
Release | : 1962 |
Genre | : |
ISBN | : |
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Author | : Robert Ples Humphreys |
Publisher | : |
Total Pages | : 90 |
Release | : 1962 |
Genre | : |
ISBN | : |
Author | : Virgil A. Sandborn |
Publisher | : |
Total Pages | : 20 |
Release | : 1962 |
Genre | : Aerodynamics |
ISBN | : |
Author | : Charles William Mautz |
Publisher | : |
Total Pages | : 276 |
Release | : 1949 |
Genre | : |
ISBN | : |
Author | : Frederick William Geiger |
Publisher | : |
Total Pages | : 216 |
Release | : 1949 |
Genre | : Transportation |
ISBN | : |
Author | : Aerospace Corporation |
Publisher | : |
Total Pages | : 86 |
Release | : 1962 |
Genre | : Shock tubes |
ISBN | : |
Author | : Robert L. Trimpi |
Publisher | : |
Total Pages | : 674 |
Release | : 1955 |
Genre | : Gas flow |
ISBN | : |
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 | : N. Muniswamy Reddy |
Publisher | : |
Total Pages | : 28 |
Release | : 1969 |
Genre | : Measurement |
ISBN | : |
Shock tube flow analysis with dimensionless velocity number.
Author | : Richard W. Ziemer |
Publisher | : |
Total Pages | : 52 |
Release | : 1958 |
Genre | : Electromagnetic waves |
ISBN | : |
An electromagnetically driven shock tube was studied as a possible new tool for aerodynamic research in which velocities of up to 41,000 feet per second are obtainable in air. At these high velocities stagnation temperatures of about 35,000K are produced. The simple construction and operation of the shock tube is described and an evaluation is made of its performance. The potentialities and limitations of the apparatus are discussed with regards to research applications. The results of some magnetoaerodynamic studies are presented to show the usefulness of this type of shock tube. (Author).
Author | : Virgil A. Sandborn |
Publisher | : |
Total Pages | : 0 |
Release | : 1962 |
Genre | : |
ISBN | : |
Author | : Irving Israel Glass |
Publisher | : University of Toronto Press |
Total Pages | : 852 |
Release | : 1970-12-15 |
Genre | : Education |
ISBN | : 1487597584 |
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.