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| Author | : Virgil A. Sandborn |
| Publisher | : |
| Total Pages | : 20 |
| Release | : 1962 |
| Genre | : Aerodynamics |
| ISBN | : |
| Author | : Anatol Roshko |
| Publisher | : |
| Total Pages | : |
| Release | : 1960 |
| Genre | : |
| ISBN | : |
| Author | : Virgil A. Sandborn |
| Publisher | : |
| Total Pages | : 0 |
| Release | : 1962 |
| Genre | : |
| ISBN | : |
| Author | : Virgil A. Sandborn |
| Publisher | : |
| Total Pages | : 15 |
| Release | : 1962 |
| Genre | : |
| ISBN | : |
| Author | : Aerospace Corporation |
| Publisher | : |
| Total Pages | : 86 |
| Release | : 1962 |
| Genre | : Shock tubes |
| ISBN | : |
| Author | : N. Muniswamy Reddy |
| Publisher | : |
| Total Pages | : 28 |
| Release | : 1969 |
| Genre | : Measurement |
| ISBN | : |
Shock tube flow analysis with dimensionless velocity number.
| 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 | : Robert L. Trimpi |
| Publisher | : |
| Total Pages | : 682 |
| Release | : 1958 |
| Genre | : Attenuation (Physics) |
| ISBN | : |
The linearized attenuation theory of NACA Technical Note 3375 is modified in the following manner: (a) an unsteady compressible local skin-friction coefficient is employed rather than the equivalent steady-flow incompressible coefficient; (b) a nonlinear approach is used to permit application of the theory to large attenuations; and (c) transition effects are considered. Curves are presented for predicting attenuation for shock pressure ratios up to 20 and a range of shock-tube Reynolds numbers. Comparison of theory and experimental data for shock wave strengths between 1.5 and 10 over a wide range of Reynolds numbers shows good agreement with the nonlinear theory evaluated for a transition Reynolds nuniber of 2.5 million.
| 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.
| Author | : Robert Ples Humphreys |
| Publisher | : |
| Total Pages | : 90 |
| Release | : 1962 |
| Genre | : |
| ISBN | : |
