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Book Theories and Technologies of Hypervelocity Shock Tunnels

Download or read book Theories and Technologies of Hypervelocity Shock Tunnels written by Zonglin Jiang and published by Cambridge University Press. This book was released on 2023-10-26 with total page 316 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

Book Theories and Technologies of Hypervelocity Shock Tunnels

Download or read book Theories and Technologies of Hypervelocity Shock Tunnels written by Zonglin Jiang and published by Cambridge University Press. This book was released on 2023-10-26 with total page 315 pages. Available in PDF, EPUB and Kindle. Book excerpt: A comprehensive reference on the basics, physics, design methods, and testing of various state-of-the art hypervelocity shock tunnels.

Book A 1 foot Hypervelocity Shock Tunnel in which High enthalpy  Real gas Air Flows Can be Generated with Flow Times of about 180 Milliseconds

Download or read book A 1 foot Hypervelocity Shock Tunnel in which High enthalpy Real gas Air Flows Can be Generated with Flow Times of about 180 Milliseconds written by Bernard E. Cunningham and published by . This book was released on 1962 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 620 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Shock Waves   Marseille I

    Book Details:
  • Author : Raymond Brun
  • Publisher : Springer Science & Business Media
  • Release : 2012-12-06
  • ISBN : 3642788297
  • Pages : 497 pages

Download or read book Shock Waves Marseille I written by Raymond Brun and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 497 pages. Available in PDF, EPUB and Kindle. Book excerpt: Recently, there have been significant advances in the fields of high-enthalpy hypersonic flows, high-temperature gas physics, and chemistry shock propagation in various media, industrial and medical applications of shock waves, and shock-tube technology. This series contains all the papers and lectures of the 19th International Symposium on Shock Waves held in Marseille in 1993. They are published in four topical volumes, each containing papers on related topics, and preceded by an overview written by a leading international expert. The volumes may be purchased independently.

Book A THEORETICAL ANALYSIS OF THE DRIVERRESERVOIR METHOD OF DRIVING HYPERSONIC SHOCK TUNNELS

Download or read book A THEORETICAL ANALYSIS OF THE DRIVERRESERVOIR METHOD OF DRIVING HYPERSONIC SHOCK TUNNELS written by Canada. Defence Research Board and published by . This book was released on 1964 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt: The driver-reservoir method of extending the test time of a tailored hypersonic shock tunnel by using a reservoir and a nozzle (perforated plate) at the upstream end of the driver is treated theoretically. It is shown that the flow following the rupture of the diaphragm is highly complex and contains both steady and unsteady flow regimes. It is also shown that the area ratio of the nozzle separating the driver from the reservoir determines the nature of the wave system produced. For a unique or 'ideal' nozzle area ratio a flow system is produced which contains no downstream running disturbances other than Mach waves. That is, both the head and the tail of the initial rarefaction wave are prevented from interfering with the shock-tunnel reservoir. Consequently, the running time of the shock tunnel can be extended. The ideal area ratios are calculated for a wide range of shock tunnel operating conditions and compared with experimental results. The comparison shows that the ideal nozzle area ratio can be predicted accurately from theory. (Author).

Book Low density Research in the Hypersonic Shock Tunnel

Download or read book Low density Research in the Hypersonic Shock Tunnel written by Charles E. Wittliff and published by . This book was released on 1960 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1963 with total page 824 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Comparison of Hotshot Tunnel Force  Pressure Heat transfer and Shock Shape Data with Shock Tunnel Data

Download or read book Comparison of Hotshot Tunnel Force Pressure Heat transfer and Shock Shape Data with Shock Tunnel Data written by E. E. Edenfield and published by . This book was released on 1964 with total page 40 pages. Available in PDF, EPUB and Kindle. Book excerpt: Comparison is made of force, pressure, heat-transfer, and shock shape data from tests in the AEDC-VKF hotshot tunnels and in the Cornell Aeronautical Laboratory 48 Inch Shock Tunnel. Several cone models of varying bluntness were tested through an angle-of-attack range of 0 to 40 deg at each facility. Excellent agreement of the hotshot and the shock tunnel data is shown. (Author).

Book Shock Tunnel Studies of High enthalpy Ionized Airflows

Download or read book Shock Tunnel Studies of High enthalpy Ionized Airflows written by Alan Eschenroeder and published by . This book was released on 1962 with total page 78 pages. Available in PDF, EPUB and Kindle. Book excerpt: Recent interest in phenomena associated with objects entering the earth's atmosphere at high velocities has stimulated research in the field of nonequilibrium flows. In many cases a more detailed knowledge of physico-chemical processes is needed than for purely aerodynamic effects because many of the composition changes which have negligible influence on the energetics of the flow may be significant in controlling the electromagnetic properties of the gas.

Book A 1 foot Hypervelocity Shock Tunnel in which High enthalpy  Real gas Air Flows Can be Generated with Flow Times of about 180 Milliseconds

Download or read book A 1 foot Hypervelocity Shock Tunnel in which High enthalpy Real gas Air Flows Can be Generated with Flow Times of about 180 Milliseconds written by Bernard E. Cunningham and published by . This book was released on 1962 with total page 43 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Hypersonic Research in the Shock Tunnel

Download or read book Hypersonic Research in the Shock Tunnel written by Charles E. Wittliff and published by . This book was released on 1960 with total page 118 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Hypersonic and High Temperature Gas Dynamics

Download or read book Hypersonic and High Temperature Gas Dynamics written by John David Anderson and published by AIAA. This book was released on 1989 with total page 710 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book is a self-contained text for those students and readers interested in learning hypersonic flow and high-temperature gas dynamics. It assumes no prior familiarity with either subject on the part of the reader. If you have never studied hypersonic and/or high-temperature gas dynamics before, and if you have never worked extensively in the area, then this book is for you. On the other hand, if you have worked and/or are working in these areas, and you want a cohesive presentation of the fundamentals, a development of important theory and techniques, a discussion of the salient results with emphasis on the physical aspects, and a presentation of modern thinking in these areas, then this book is also for you. In other words, this book is designed for two roles: 1) as an effective classroom text that can be used with ease by the instructor, and understood with ease by the student; and 2) as a viable, professional working tool for engineers, scientists, and managers who have any contact in their jobs with hypersonic and/or high-temperature flow.

Book Shock Tunnel Studies on Lateral Jets  Hypervelocity Cross Flow Interaction

Download or read book Shock Tunnel Studies on Lateral Jets Hypervelocity Cross Flow Interaction written by and published by . This book was released on 1997 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Shock Waves   Marseille I

    Book Details:
  • Author : Raymond Brun
  • Publisher : Springer
  • Release : 1995-05-10
  • ISBN : 9783540577102
  • Pages : 485 pages

Download or read book Shock Waves Marseille I written by Raymond Brun and published by Springer. This book was released on 1995-05-10 with total page 485 pages. Available in PDF, EPUB and Kindle. Book excerpt: Recently, there have been significant advances in the fields of high-enthalpy hypersonic flows, high-temperature gas physics, and chemistry shock propagation in various media, industrial and medical applications of shock waves, and shock-tube technology. This series contains all the papers and lectures of the 19th International Symposium on Shock Waves held in Marseille in 1993. They are published in four topical volumes, each containing papers on related topics, and preceded by an overview written by a leading international expert. The volumes may be purchased independently.