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Double Shock Tube Method For Simultaneous Determination Of High Pressure And Temperature Of An Enclosed Gas
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Book Synopsis Double Shock Tube Method for Simultaneous Determination of High Pressure and Temperature of an Enclosed Gas by : W. R. Grabowsky
Download or read book Double Shock Tube Method for Simultaneous Determination of High Pressure and Temperature of an Enclosed Gas written by W. R. Grabowsky and published by . This book was released on 1964 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt: A method is discussed for the simultaneous determination of pressure and temperature of a confined, impulsively heated gas. The method requires the measurement of the shock Mach numbers in two small shock tubes that use the impulsively heated gas as a driver. Different initial pressures in the shock tubes result in two simultaneous equations for driver pressure and temperature as a function of the measured shock Mach numbers. These equations are examined for ideal and real gases in the limit of infinite driver to driven section area ratio. The effect of contamination of the driver gas during the heating pulse is considered also. (Author).
Book Synopsis Scientific and Technical Aerospace Reports by :
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 716 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis U.S. Government Research Reports by :
Download or read book U.S. Government Research Reports written by and published by . This book was released on 1964 with total page 2180 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Shock Tube in High-temperature Chemical Physics by : Alfred Gordon Gaydon
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 344 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Shock-tube Flow Analysis with a Dimensionless Velocity Number by : N. Muniswamy Reddy
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.
Book Synopsis Measurement of Frequency Response of Pressure Gauges by a High-pressure Shock Tube Technique by : S. P. Pfaff
Download or read book Measurement of Frequency Response of Pressure Gauges by a High-pressure Shock Tube Technique written by S. P. Pfaff and published by . This book was released on 1958 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis A Digital Computer Program for Calculating the Performance of Single-or Multiple-diaphragm Shock Tubes for Arbitrary Equilibrium Real Gas Mixtures by : William L. Grose
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:
Book Synopsis A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification by : Robert L. Trimpi
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.
Book Synopsis Performance of an Opposed Flow Shock Tube for the Measurement of Gas Thermal Conductivity by : William G. Steenken
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:
Book Synopsis Shock Tube and Gas Dynamic Design Considerations and Implementation for Extended Test Times by : Jacklyn Higgs
Download or read book Shock Tube and Gas Dynamic Design Considerations and Implementation for Extended Test Times written by Jacklyn Higgs and published by . This book was released on 2022 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new shock tube test section has been designed and manufactured for the purpose of increasing the test time and expanding the applications of the shock tube for a multitude of ongoing and future projects. One purpose for the test section extension is to allow for flow visualization of droplets impacted by a shock wave for the interaction of hypersonic vehicles and atmospheric disturbances. Another purpose is to measure behind the incident shock to capture the chemical kinetics for a high-altitude environment and low-pressure, high-temperature space applications. This new test section contains 24 round optical ports for laser spectroscopy for multiple measurement locations in addition to 3 rectangular ports upstream for introducing and imaging droplets in the tube. StanShock was used to simulate the expected test time for the desired temperatures and pressures. This was compared against theoretical calculations of test time as a function of distance and velocity of the shock. The optimal length of the extension of 5 feet was then determined based on minimum required test time and limitations of the physical lab space.
Book Synopsis Strategies for Obtaining Long Constant-pressure Test Times in Shock Tubes by :
Download or read book Strategies for Obtaining Long Constant-pressure Test Times in Shock Tubes written by and published by . This book was released on 2015 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt: Several techniques have been developed for obtaining long, constant-pressure test times in reflected shock wave experiments in a shock tube, including the use of driver inserts, driver gas tailoring, helium gas diaphragm interfaces, driver extensions, and staged driver gas filling. Here, we detail these techniques, including discussion on the most recent strategy, staged driver gas filling. Experiments indicate that this staged filling strategy increases available test time by roughly 20 % relative to single-stage filling of tailored driver gas mixtures, while simultaneously reducing the helium required per shock by up to 85 %. This filling scheme involves firstly mixing a tailored helium-nitrogen mixture in the driver section as in conventional driver filling and, secondly, backfilling a low-speed-of-sound gas such as nitrogen or carbon dioxide from a port close to the end cap of the driver section. Using this staged driver gas filling, in addition to the other techniques listed above, post-reflected shock test times of up to 0.102 s (102 ms) at 524 K and 1.6 atm have been obtained. Spectroscopically based temperature measurements in non-reactive mixtures have confirmed that temperature and pressure conditions remain constant throughout the length of these long test duration trials. Finally, these strategies have been used to measure low-temperature n-heptane ignition delay times.
Author :United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch Publisher : ISBN 13 : Total Pages :1080 pages Book Rating :4.E/5 ( download)
Book Synopsis Japanese Science and Technology, 1983-1984 by : United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Download or read book Japanese Science and Technology, 1983-1984 written by United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch and published by . This book was released on 1985 with total page 1080 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis 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 by : Jim J. Jones
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:
Book Synopsis Bibliography of Scientific and Industrial Reports by :
Download or read book Bibliography of Scientific and Industrial Reports written by and published by . This book was released on 1964 with total page 1420 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1964 with total page 538 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Temperature Calibration of the High Pressure Single Pulse Shock Tube at Relatively Low Pressures by : Hari Ramamoorthy
Download or read book Temperature Calibration of the High Pressure Single Pulse Shock Tube at Relatively Low Pressures written by Hari Ramamoorthy and published by . This book was released on 2002 with total page 210 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis The Use of Real Gases in a Shock Tube by : Russell Earl Duff
Download or read book The Use of Real Gases in a Shock Tube written by Russell Earl Duff and published by . This book was released on 1951 with total page 290 pages. Available in PDF, EPUB and Kindle. Book excerpt:
