Download or read book Performance of an Opposed Flow Shock Tube for the Measurement of Gas Thermal Conductivity written by William G. Steenken and published by . This book was released on 1967 with total page 230 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Shock tube Flow Analysis with a Dimensionless Velocity Number written by N. Muniswamy Reddy and published by . This book was released on 1969 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: Shock tube flow analysis with dimensionless velocity number.

Download or read book A Digital Computer Program for Calculating the Performance of Single or Multiple diaphragm Shock Tubes for Arbitrary Equilibrium Real Gas Mixtures written by William L. Grose and published by . This book was released on 1968 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification written by Robert L. Trimpi and published by . This book was released on 1955 with total page 674 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Download or read book Shock Tubes and Waves written by Charles E. Treanor and published by State University of New York Press. This book was released on 1982-06-30 with total page 908 pages. Available in PDF, EPUB and Kindle. Book excerpt: Sponsored by the U.S. Air Force Office of Scientific Research, this conference was held in Niagara Falls on July 6–9, 1981. This book includes material on the following topics: instrumentation and diagnostics, shock tube facilities and techniques, gas dynamic experiments, heat transfer and real gas effects, boundary layers, shock structure, shock propagation, laser and spectral optical studies, chem and kinetics, relaxation and excitation, ionization, dusty gases, two-phase flow and condensation, shock waves in the environment and energy, and energy-related processes. The book contains a total of 98 papers by well-known specialists.

Download or read book Shock tube Study of the Transient Thermal Behavior of Gases at High temperature written by Stanford University. Department of Aeronautics and Astronautics and published by . This book was released on 1969 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Evaluation of Expansion Chambers in Shock Tubes written by Horst P. Richter and published by . This book was released on 1969 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Shock Tube Investigation of Thermal Conductivity in Noble Gases written by Federico A. Penaranda and published by . This book was released on 1969 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: A shock tube was developed and instrumented. The shock tube was used in an experiment in which the thermal conductivity of argon was determined in the temperature range of 1500 - 5000K and at relatively high pressures, 10 to 30 atmospheres. (Author).

Download or read book Shock tube Heat transfer Measurements on Inner Surface of a Cylinder simulating a Flat Plate for Stagnation temperature Range 4 100 to 8 300 R written by Jim J. Jones and published by . This book was released on 1959 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Partial Performance Features of the Wisconsin High Enthalpy Shock Tube written by Charles Wilfred Fisher and published by . This book was released on 1966 with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book The Shock Tube in High temperature Chemical Physics written by Alfred Gordon Gaydon and published by . This book was released on 1963 with total page 338 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Measurement of Wall Heat Transfer and of Transitions to Turbulence During Hot Gas and Rarefaction Flows in a Shock Tube written by Albert John Chabai and published by . This book was released on 1958 with total page 172 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Shock Tube Study of the Coefficient of Thermal Conductivity of Helium Neon Argon and Krypton written by Peter Jozef Vrugt and published by . This book was released on 1976 with total page 107 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Shock tube measurements of thermal accommodation between a hot gas and a cold solid written by R. K. Hanson and published by . This book was released on 1970 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Shock tube Measurements of Thermal Accomodation Between a Hot Gas and a Cold Solid written by R. K. Hanson and published by . This book was released on 1970 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Download or read book Measurements in a Shock Tube of Heat Transfer Rates at the Stagnation Point of a 1 0 inch diameter Sphere for Real gas Temperatures Up to 7 900 Degrees R written by Alexander P. Sabol and published by . This book was released on 1958 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat-transfer rates at the stagnation point of 1.0-inch-diameter glass spherical models have been measured in shock-tube flows in air which corresponded to free-flight conditions between Mach numbers of 6.4 and 13.9 with stagnation temperatures up to 7,900 degrees R. The heat-transfer rates were determined from measurements of the surface-temperature change with time of a thin-film-platinum resistance thermometer. Test results are presented and compared with the results from the theories of Lees (Jet Propulsion, April 1956) and Fay and Riddell (AVCO Research Report 1). The experimental results obtained give lower heat-transfer rates than both theories but are more compatible with results from the theory of Lees. These test results are also compared with thermocouple data and with the results obtained by the use of similar configurations.

Download or read book Experimental Determination of the Transport Properties of Gases Part Ii Heat Transfer and Ultrasonic Measurements written by Charles A. Carey and published by . This book was released on 1966 with total page 96 pages. Available in PDF, EPUB and Kindle. Book excerpt: Methods of experimentally determining the transport properties of high temperature gases have been developed and measurements of viscosity, thermal conducitvity, and diffusion coefficients obtained. The heat transfer rate through laminar boundary layers, the absorption of sound, and a schlieren method have been investigated for the determination of transport properties. Heat transfer measurements on the side wall of the shock tube have been used to obtain viscosities of argon, oxygen, nitrogen, and carbon dioxide up to 4000 K. The boundary layer equations were solved for side wall boundary layers in the shock tube in oxygen to assess the relative importance of viscosity and thermal conductivity in heat transfer to the side wall. Thermal conductivities were deduced from end wall heat transfer measurements in carbon dioxide up to 2000 K and oxygen up to 4000 K. End wall heat transfer measurements in nitrogen and argon have been compared to theory with excellent agreement. Various methods for measuring ultrasonic absorption are discussed. The viscosity of argon at temperatures up to 8000 K were determined with the ultrasonic method. Diffusion coefficient in 50-50 He-Ar mixtures have also been obtained from the ultrasonic measurements at room temperature with excellent agreement with other investigators. The theory of a schlieren method for the measurement of thermal conductivity using the end wall boundary layer in the shock tube is discussed. (Author).