Theories And Technologies Of Hypervelocity Shock Tunnels
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Theories and Technologies of Hypervelocity Shock Tunnels by Zonglin Jiang,Randy S. M. Chue Pdf
Introducing the state-of-the-art of hypervelocity shock tunnels, this complete reference features a variety of drivers and step-by-step introductions to their theories, physics, methods and testing. This book enables researchers and engineers in aerospace to design and improve wind tunnels that simulate flow qualities of real hypersonic flyers.
Experimental Methods of Shock Wave Research by Ozer Igra,Friedrich Seiler Pdf
This comprehensive and carefully edited volume presents a variety of experimental methods used in Shock Waves research. In 14 self contained chapters this 9th volume of the “Shock Wave Science and Technology Reference Library” presents the experimental methods used in Shock Tubes, Shock Tunnels and Expansion Tubes facilities. Also described is their set-up and operation. The uses of an arc heated wind tunnel and a gun tunnel are also contained in this volume. Whenever possible, in addition to the technical description some typical scientific results obtained using such facilities are described. Additionally, this authoritative book includes techniques for measuring physical properties of blast waves and laser generated shock waves. Information about active shock wave laboratories at different locations around the world that are not described in the chapters herein is given in the Appendix, making this book useful for every researcher involved in shock/blast wave phenomena.
Investigations in Soviet Hypervelocity Testing Technique by Library of Congress. Aerospace Technology Division Pdf
This comprehensive report is based on Soviet-Satellite open sources published 1924-1965. It concerns experimental research in high velocity aerodynamics and gas dynamics. The first section lists facilities and personnel engaged in this field of research; it gives data on wind tunnels, shock tubes, and shock tube flows; a third chapter pertains to measurement techniques (velocity, density, temperature, and pressure). The second section deals with such problems of aerophysics as the state of a gas heated by a shock wave and related phenomena taking place behind a shock wave, such as dissociation, ionization, light emission, radiation, and formation of plasma. It includes chapters on shock tube flows, boundary layer interaction, physical properties of gases at high temperatures, heat transfer, mass transfer, and detonation. The research is based on simulation of the conditions encountered in space flights and reentry by creating highspeed, high-temperature ionized gas flows by means of shock waves produced in supersonic wind tunnels, shock tubes, discharge tubes, and by explosions. Emphasis has been placed on supersonic shock tube investigations. The shock wave methods employed in laboratory studies of the physical and physiochemical properties of various gases heated by shock waves at high temperatures, the specific apparatus, and the auxiliary means characteristic of many laboratories are described. (Author).
NASA Scientific and Technical Publications: A Catalog of Special Publications, Reference Publications, Conference Publications, and Technical Papers, 1991-1992 by Anonim Pdf
