Measurements of Flow Duration in a Low-pressure Shock Tube
Author: Virgil A. Sandborn
Publisher:
Published: 1962
Total Pages: 20
ISBN-13:
DOWNLOAD EBOOKRead and Download eBook Full
Author: Virgil A. Sandborn
Publisher:
Published: 1962
Total Pages: 20
ISBN-13:
DOWNLOAD EBOOKAuthor: Anatol Roshko
Publisher:
Published: 1960
Total Pages:
ISBN-13:
DOWNLOAD EBOOKAuthor: Virgil A. Sandborn
Publisher:
Published: 1962
Total Pages: 15
ISBN-13:
DOWNLOAD EBOOKAuthor: Aerospace Corporation
Publisher:
Published: 1962
Total Pages: 86
ISBN-13:
DOWNLOAD EBOOKAuthor: N. Muniswamy Reddy
Publisher:
Published: 1969
Total Pages: 28
ISBN-13:
DOWNLOAD EBOOKShock tube flow analysis with dimensionless velocity number.
Author: Robert L. Trimpi
Publisher:
Published: 1955
Total Pages: 674
ISBN-13:
DOWNLOAD EBOOKThe 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 Ples Humphreys
Publisher:
Published: 1962
Total Pages: 90
ISBN-13:
DOWNLOAD EBOOKAuthor: Irving Israel Glass
Publisher: University of Toronto Press
Published: 1970-12-15
Total Pages: 852
ISBN-13: 1487597584
DOWNLOAD EBOOKThis 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 L. Trimpi
Publisher:
Published: 1958
Total Pages: 682
ISBN-13:
DOWNLOAD EBOOKThe 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.