Experimental Study of the Starting Process, Flow Duration, and Nozzle Boundary Layer in a High-enthalpy Shock Tunnel
Author | : Michael G. Dunn |
Publisher | : |
Total Pages | : 92 |
Release | : 1967 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
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Author | : Michael G. Dunn |
Publisher | : |
Total Pages | : 92 |
Release | : 1967 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : |
Author | : Michael G. Dunn |
Publisher | : |
Total Pages | : 146 |
Release | : 1969 |
Genre | : Space vehicles |
ISBN | : |
Author | : BALLMAN |
Publisher | : Springer Science & Business Media |
Total Pages | : 448 |
Release | : 2012-12-06 |
Genre | : Technology & Engineering |
ISBN | : 1461203791 |
These three volumes entitled Advances in Hypersonics contain the Proceedings of the Second and Third Joint US/Europe Short Course in Hypersonics which took place in Colorado Springs and Aachen. The Second Course was organized at the US Air Force Academy, USA in January 1989 and the Third Course at Aachen, Germany in October 1990. The main idea of these Courses was to present to chemists, com puter scientists, engineers, experimentalists, mathematicians, and physicists state of the art lectures in scientific and technical dis ciplines including mathematical modeling, computational methods, and experimental measurements necessary to define the aerothermo dynamic environments for space vehicles such as the US Orbiter or the European Hermes flying at hypersonic speeds. The subjects can be grouped into the following areas: Phys ical environments, configuration requirements, propulsion systems (including airbreathing systems), experimental methods for external and internal flow, theoretical and numerical methods. Since hyper sonic flight requires highly integrated systems, the Short Courses not only aimed to give in-depth analysis of hypersonic research and technology but also tried to broaden the view of attendees to give them the ability to understand the complex problem of hypersonic flight. Most of the participants in the Short Courses prepared a docu ment based on their presentation for reproduction in the three vol umes. Some authors spent considerable time and energy going well beyond their oral presentation to provide a quality assessment of the state of the art in their area of expertise as of 1989 and 1991.
Author | : S. N. B. Murthy |
Publisher | : AIAA |
Total Pages | : 558 |
Release | : 1991 |
Genre | : Aerodynamics, Hypersonic |
ISBN | : 9781600863912 |
Annotation Leading researchers provide a cohesive treatment of the complex issues in high-speed propulsion, as well as introductions to the current capabilities for addressing several fundamental aspects of high-speed vehicle propulsion development. Includes more than 380 references, 290 figures and tables, and 185 equations.
Author | : Ozer Igra |
Publisher | : Springer |
Total Pages | : 480 |
Release | : 2015-10-31 |
Genre | : Technology & Engineering |
ISBN | : 3319237454 |
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.