Phenomena in Supersonic Diffusers
Author | : Heinrich Ramm |
Publisher | : |
Total Pages | : 34 |
Release | : 1947 |
Genre | : Supersonic diffusers |
ISBN | : |
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Author | : Heinrich Ramm |
Publisher | : |
Total Pages | : 34 |
Release | : 1947 |
Genre | : Supersonic diffusers |
ISBN | : |
Author | : Howard W. Emmons |
Publisher | : Princeton University Press |
Total Pages | : 784 |
Release | : 2015-12-08 |
Genre | : Science |
ISBN | : 1400877539 |
Volume II of the High Speed Aerodynamics and Jet Propulsion series. The series which stress the more fundamental aspects of the various phenomena that make up the broad field of aeronautical science. The aerodynamicist and gas dynamicist will find both the classical and the important new concepts of gas dynamics presented in an informative and stimulating manner. Specialists in the study of gas dynamics have contributed Sections as follows: H. S. Tsien, The Equations of Gas Dynamics; L. Crocco, One-Dimensional Treatment of Steady Gas Dynamics; A. Kantrowitz, One-Dimensional Treatment of Nonsteady Gas Dynamics; W. Hayes, The Basic Theory of Gasdynamic Discontinuities; H. Polachek and R. J. Seeger, Shock Wave Interactions; H. G. Stever, Condensation Phenomena in High Speed Flows; T. H. Von Karman, H. W. Emmons, G. I. Taylor, and R. S. Tankin, Gas Dynamics of Combustion and Detonation; S. Schaaf and P. Chambre, Flow of Rarefied Gases. Originally published in 1958. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.
Author | : Gabi Ben-Dor |
Publisher | : Springer |
Total Pages | : 746 |
Release | : 2017-08-09 |
Genre | : Technology & Engineering |
ISBN | : 331946213X |
These proceedings collect the papers presented at the 30th International Symposium on Shock Waves (ISSW30), which was held in Tel-Aviv Israel from July 19 to July 24, 2015. The Symposium was organized by Ortra Ltd. The ISSW30 focused on the state of knowledge of the following areas: Nozzle Flow, Supersonic and Hypersonic Flows with Shocks, Supersonic Jets, Chemical Kinetics, Chemical Reacting Flows, Detonation, Combustion, Ignition, Shock Wave Reflection and Interaction, Shock Wave Interaction with Obstacles, Shock Wave Interaction with Porous Media, Shock Wave Interaction with Granular Media, Shock Wave Interaction with Dusty Media, Plasma, Magnetohyrdrodynamics, Re-entry to Earth Atmosphere, Shock Waves in Rarefied Gases, Shock Waves in Condensed Matter (Solids and Liquids), Shock Waves in Dense Gases, Shock Wave Focusing, Richtmyer-Meshkov Instability, Shock Boundary Layer Interaction, Multiphase Flow, Blast Waves, Facilities, Flow Visualization, and Numerical Methods. The two volumes serve as a reference for the participants of the ISSW30 and anyone interested in these fields.
Author | : M. Champion |
Publisher | : Springer Science & Business Media |
Total Pages | : 413 |
Release | : 2012-12-06 |
Genre | : Science |
ISBN | : 9401154325 |
Proceedings of the IUTAM Symposium held in Poitiers, France, 2-6 October 1995
Author | : John R. Spreiter |
Publisher | : |
Total Pages | : 646 |
Release | : 1949 |
Genre | : Aerodynamic load |
ISBN | : |
The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic speeds.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1200 |
Release | : 1954 |
Genre | : Aeronautics |
ISBN | : |
Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.
Author | : United States. National Advisory Committee for Aeronautics |
Publisher | : |
Total Pages | : 1498 |
Release | : 1953 |
Genre | : Aeronautics |
ISBN | : |
Author | : Aeronautical Research Council (Great Britain) |
Publisher | : |
Total Pages | : 588 |
Release | : 1961 |
Genre | : Aeronautics |
ISBN | : |
Includes its Reports, which are also issued separately.