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Author : Gerald Allan Oberlag
Publisher :
ISBN 13 :
Total Pages : 148 pages
Book Rating : 4.:/5 (123 download)
Download or read book Design and Instrumentation of a Shock Tube written by Gerald Allan Oberlag and published by . This book was released on 1967 with total page 148 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : I. I. Glass
Publisher :
ISBN 13 :
Total Pages : 259 pages
Book Rating : 4.:/5 (263 download)
Download or read book Shock Tubes written by I. I. Glass and published by . This book was released on 1958 with total page 259 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : J. Gordon Hall
Publisher :
ISBN 13 :
Total Pages : 259 pages
Book Rating : 4.:/5 (977 download)
Download or read book Shock Tubes. Part II written by J. Gordon Hall and published by . This book was released on 1958 with total page 259 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : B. P. Polanin
Publisher :
ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)
Download or read book Design and Instrumentation of an Earth Shock Tube written by B. P. Polanin and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: A system to measure the friction at the sidewall of the earth shock tube has been designed. Four Baldwin-LimaHamilton load cells, one attached at each corner of a flange, will support the suspended shock tube, and hence will indicate the total downward force exerted on the shock tube during application of force to the soil column.
Author : R. Hide
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (897 download)
Download or read book The Design, Construction, Instrumentation and Performance of an 8 X 2 Inch Shock Tube written by R. Hide and published by . This book was released on 1962 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Bernard Polanin
Publisher :
ISBN 13 :
Total Pages : 216 pages
Book Rating : 4.:/5 (227 download)
Download or read book Design and Instrumentation of an Earth Shock Tube written by Bernard Polanin and published by . This book was released on 1968 with total page 216 pages. Available in PDF, EPUB and Kindle. Book excerpt: The major objective was to design an instrumented earth shock tube for one-dimensional propagation. Ideally, the lateral strains should not interfere with the axial motion of the soil particles. However, the side friction was too great. Therefore, Teflon powder between the soil sample and the confining tube was used to reduce friction. Testing of this system indicated that imbedded stress gage behavior should be explored before further testing of the earth shock tube. Two laboratory devices - the dynamic oedometer and the dynamic triaxial apparatus were designed for looking at stress gage behavior and one-dimensional soil constants. Although results were obtained, further investigations are required to complete the evaluation of the above system. An earth strain gage and a horizontal displacement meter were developed. (Author).
Author : United Kingdom Atomic Energy Authority. Research Group
Publisher :
ISBN 13 :
Total Pages : 27 pages
Book Rating : 4.:/5 (32 download)
Download or read book The Design, Construction, Instrumentation and Performance of an 8 X 2 Inch Shock Tube written by United Kingdom Atomic Energy Authority. Research Group and published by . This book was released on 1962 with total page 27 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Constantine Gregory Avgoustopoulos
Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.:/5 (12 download)
Download or read book The Design, Instrumentation, and Validation of a Multiphase Shock Tube Facility written by Constantine Gregory Avgoustopoulos and published by . This book was released on 2017 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper investigates the experimental work in Shock Driven Multiphase Instabilities (SDMI). SDMIs occur when an interface consisting of a particle seeded gas is instantaneously accelerated and begins mixing. SDMIs have similar flow morphologies to the Richtmyer-Meshkov Instability (RMI), however, the driving force inducing this flow is very different. SDMIs occur when there is a relative velocity difference between surrounding gas and the moving particles. This results to a shear at the edges and ultimately leads to rollups that are similar to a RMI. To investigate this phenomena, a shock tube facility was designed, calibrated, and tested to perform experiments. The experimental data was qualitatively compared to simulations performed, as well as to literature of similar experiments. Quantitative data was analyzed using Particle Imaging Velocimetry (PIV) to understand the flow of the instability. The flow morphologies observed in experiments have similar behavior to those performed in simulations. Additionally, the qualitative observations of experiments performed in this lab are also in agreement with experimental literature. Two different effective Atwood numbers are investigated in this study. The first case looks at a gas cylinder interface with an effective Atwood number of -0.01 and a gas Atwood number of -0.02, shocked with a Mach 1.66 shock wave. The observations show a dominating instability resulting in the gas Atwood number. What ends up happening is the smaller particles are pulled into the vortex and the large particles separate and trail behind. The second case looks at the same gas cylinder perturbation but with an effective Atwood number of 0.03 and a gas Atwood number of 0, shocked at Mach 1.66. The higher Atwood number was achieved by modifying the experimental apparatus slightly to deliver a greater number of particles to the shock tube. The experiments observed show that there is agreement with literature and simulations. Certain unusual filaments begin forming at late times, 4.0ms after shock. This was thought to only appear in a pure RMI. In the case of a SDMI, these filaments are a result of colliding particles.
Author : James Everett West
Publisher :
ISBN 13 :
Total Pages : 176 pages
Book Rating : 4.:/5 (599 download)
Download or read book Instrumentation of a Shock Tube Facility written by James Everett West and published by . This book was released on 1968 with total page 176 pages. Available in PDF, EPUB and Kindle. Book excerpt: "The theory of schlieren and interferometer systems was described and related to studies of shock waves in a shock tube. An interferometer was procured and a schlieren system was modified for use with the UMR shock tube facility. The design and construction of a base for the systems and window assemblies for the shock tube comprised the major portion of the work on this project. A short series of tests were run to ascertain the compatibility of the instrumentation to the UMR shock tube facility. While no schlieren photograph of the shock wave was obtained, the system was shown to be operating properly. The piezoelectric pressure transducers used in conjunction with a dual beam oscilloscope provided a record from which shock velocity and strength could be calculated. Test results were compared were possible to theoretical values and very good correlation was obtained"--Abstract, leaf ii.
Author : Frederick William Geiger
Publisher :
ISBN 13 :
Total Pages : 218 pages
Book Rating : 4.3/5 (91 download)
Download or read book The Shock Tube as an Instrument for the Investigation of Transonic and Supersonic Flow Patterns written by Frederick William Geiger and published by . This book was released on 1949 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : August J. Caponecchi
Publisher :
ISBN 13 :
Total Pages : 125 pages
Book Rating : 4.:/5 (227 download)
Download or read book The Design and Construction of a Chemical Shock Tube written by August J. Caponecchi and published by . This book was released on 1967 with total page 125 pages. Available in PDF, EPUB and Kindle. Book excerpt: The design and construction of a chemical shock tube is described. The shock tube consists of a support structure, a dump tank, a driver section, and a driven section. The time delay between breakage of two diaphragms located on either side of the driver section is controlled by varying the response times of two pneumatically operated actuators. An air operated gate valve of a novel design is used to isolate the reacted gas in a small region of the driven section. A simple, inexpensive instrumentation system for measuring shock wave velocity is presented. Unique analytical-digital techniques used in the design are included in the appendices. (Author).
Author : Charles E. Treanor
Publisher : State University of New York Press
ISBN 13 : 1438405502
Total Pages : 908 pages
Book Rating : 4.4/5 (384 download)
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.
Author : Irving Israel Glass
Publisher : University of Toronto Press
ISBN 13 : 1487597584
Total Pages : 852 pages
Book Rating : 4.4/5 (875 download)
Download or read book Shock Tubes written by Irving Israel Glass and published by University of Toronto Press. This book was released on 1970-12-15 with total page 852 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 : A. G. Boyer
Publisher :
ISBN 13 :
Total Pages : 130 pages
Book Rating : 4.:/5 (172 download)
Download or read book Design, Instrumentation and Performance of the UTIAS 4-in. X 7-in. Hypersonic Shock Tube written by A. G. Boyer and published by . This book was released on 1965 with total page 130 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Jacklyn Higgs
Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (136 download)
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.
Author : I. I. Glass
Publisher :
ISBN 13 :
Total Pages : 634 pages
Book Rating : 4.:/5 (227 download)
Download or read book Handbook of Supersonic Aerodynamics. Volume 6. Section 18. Shock Tubes written by I. I. Glass and published by . This book was released on 1959 with total page 634 pages. Available in PDF, EPUB and Kindle. Book excerpt: Contents: Performance of Simple Constant-Area Shock Tubes; Observed Flows in a Constant-Area Shock Tube; Production of Strong Shock Waves; Applications of the Shock Tube; Shock-Tube Materials, Design, and Construction; and Shock-Tube Flow Measurement and Instrumentation.
Author : Alfred Gordon Gaydon
Publisher :
ISBN 13 :
Total Pages : 344 pages
Book Rating : 4.3/5 (91 download)
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:
