Author: Virgil A. SandbornPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
Measurements of Flow Duration in a Low-pressure Shock Tube
Author: Virgil A. SandbornPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 20
Book Description
On Flow Duration in Low-pressure Shock Tubes
Author: Anatol RoshkoMeasurements of Flow Duration in a Low-pressure Shock Tube
Author: Virgil A. SandbornMeasurement of Flow Duration in a Low-pressure Shock Tube
Author: Virgil A. SandbornTest Time in Low Pressure Shock Tubes
Author: Aerospace CorporationPublisher:
ISBN:
Category : Shock tubes
Languages : en
Pages : 86
Book Description
Shock-tube Flow Analysis with a Dimensionless Velocity Number
Author: N. Muniswamy ReddyPublisher:
ISBN:
Category : Measurement
Languages : en
Pages : 28
Book Description
Shock tube flow analysis with dimensionless velocity number.
A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification
Author: Robert L. TrimpiPublisher:
ISBN:
Category : Gas flow
Languages : en
Pages : 674
Book Description
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.
A Nonlinear Theory for Predicting the Effects of Unsteady Laminar, Turbulent, Or Transitional Boundary Layers on the Attenuation of Shock Waves in a Shock Tube with Experimental Comparison
Author: Robert L. TrimpiPublisher:
ISBN:
Category : Attenuation (Physics)
Languages : en
Pages : 682
Book Description
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.
Shock Tubes
Author: Irving Israel GlassPublisher: University of Toronto Press
ISBN: 1487597584
Category : Education
Languages : en
Pages : 852
Book Description
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.
Uniform Flow Duration in Shock Tubes
Author: Robert Ples HumphreysPublisher:
ISBN:
Category :
Languages : en
Pages : 90
Book Description