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Author : Charles E. Wittliff
Publisher :
ISBN 13 :
Total Pages : 46 pages
Book Rating : 4.E/5 ( download)
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:
Author : SERGIO R. PANUNZIO
Publisher :
ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (227 download)
Download or read book Aerodynamic Analysis of a Low Density Hypersonic Shock-wind Tunnel written by SERGIO R. PANUNZIO and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Antonio Ferri
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (227 download)
Download or read book Preliminary Description of a New Scheme for a Low Density Hypersonic Shock Wind Tunnel written by Antonio Ferri and published by . This book was released on 1959 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: A preliminary analysis of the phenomenon involved in the combination of a shock tube technique and a wind tunnel is presented. It appears that such a combination can be used for tests at high speed where it is necessary to reach thermodynamic equilibrium conditions in front of the models. (Author).
Author : Shao-Chi Lin
Publisher :
ISBN 13 :
Total Pages : 30 pages
Book Rating : 4.:/5 (156 download)
Download or read book Low-density Shock Tube Studies of Reaction Rates Related to the High Altitude Hypersonic Flight Problem written by Shao-Chi Lin and published by . This book was released on 1960 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Charles F. Wittliff
Publisher :
ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.3/5 (91 download)
Download or read book Low-density Stagnation-point Heat Transfer in Hypersonic Air Flow written by Charles F. Wittliff and published by . This book was released on 1961 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: Stagnation-point heat transfer to two- and three-dimensional bodies at low Reynolds numbers was studied to obtain hypersonic low-density data and to demonstrate the suitability of the hypersonic shock tunnel as a facility for research in rarefied gasdynamics. Low-density experiments on a transverse cylinder and a hemisphere cylinder were made in air at Mach numbers from 8.4 to 11.6 in the CAL 11- by 15-inch hypersonic shock tunnel. The stagnation pressure and temperature, as well as model diameter, were varied to obtain a range of Reynolds numbers from 11 to 1000, based on flow conditions behind the bow shock wave and model radius. The experimental heat-transfer rates are presented and compared with theoretical predictions. The data obtained with the transverse cylinders are in good agreement with continuum boundary-layer theory at all but the lowest Reynolds numbers and highest Knudsen numbers. The hemisphere-cylinder data indicated the presence of a significant vorticity-interaction effect. Good agreement with the theoretical analysis of H.K. Cheng accounting for this effect is indicated.
Author : F.R. Riddell
Publisher : Elsevier
ISBN 13 : 0323142621
Total Pages : 769 pages
Book Rating : 4.3/5 (231 download)
Download or read book Hypersonic Flow Research written by F.R. Riddell and published by Elsevier. This book was released on 2012-12-02 with total page 769 pages. Available in PDF, EPUB and Kindle. Book excerpt: Progress in Astronautics and Rocketry, Volume 7: Hypersonic Flow Research compiles papers presented at a conference on hypersonics held at the Massachusetts Institute of Technology in August 1961. This book discusses the low Reynolds number effects, chemical kinetics effects, inviscid flow calculations, and experimental techniques relating to the problems in acquiring an understanding of hypersonic flow. The structure and composition of hypersonic wakes with attendant complex chemical kinetic effects is only briefly mentioned. This text consists of five parts. Parts A to C comprise of theoretical papers on the problems of calculating flow fields at hypersonic speeds. The experimental techniques that are of immediate practical interest in view of the difficulty of flight testing are discussed in Parts D and E. This publication is beneficial to engineers involved in advanced design problems.
Author : BALLMAN
Publisher : Springer Science & Business Media
ISBN 13 : 1461203791
Total Pages : 448 pages
Book Rating : 4.4/5 (612 download)
Download or read book Advances in Hypersonics written by BALLMAN and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 448 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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 : Charles E. Wittliff
Publisher :
ISBN 13 :
Total Pages : 118 pages
Book Rating : 4.E/5 ( download)
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:
Author : Christopher E. Glass
Publisher :
ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (317 download)
Download or read book Numerical Simulation of Low-Density Shock-Wave Interactions written by Christopher E. Glass and published by . This book was released on 1999 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt: CFD numerical simulations of low-density shock-wave interactions for an incident shock impinging on a cylinder have been performed. Flow-field density gradient and surface pressure and heating define the type of interference pattern and corresponding perturbations. The maximum pressure and heat transfer level and location of various interaction types are presented. A time-accurate solution of the Type IV interference is employed to demonstrate the establishment and the steadiness of the low-density flow interaction.
Author : United States. Congress. House. Committee on Science and Astronautics
Publisher :
ISBN 13 :
Total Pages : 1630 pages
Book Rating : 4.3/5 (91 download)
Download or read book Hearings written by United States. Congress. House. Committee on Science and Astronautics and published by . This book was released on 1971 with total page 1630 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : R. J. Vidal
Publisher :
ISBN 13 :
Total Pages : 79 pages
Book Rating : 4.:/5 (227 download)
Download or read book An Experimental Study of Hypersonic Low-density Viscous Effects on a Sharp Flat Plate written by R. J. Vidal and published by . This book was released on 1964 with total page 79 pages. Available in PDF, EPUB and Kindle. Book excerpt: Heat transfer and pressure data were obtained with sharp flat plate models at zero and large angles of attack in the CAL hypersonic shock tunnel. These high Mach number data (Mach 14 to 24) extend from the classical thin boundary layer regime to near-free-molecule conditions and are discussed within the framework of existing theory. The large angle-of-attack results verify viscous shock-layer theory and define the low-density conditions where transport effects at the shock wave first become important. The data obtained at zero angle of attack are compared with theory to define the fluid mechanism that governs the low-density effects. The strong shock-wave approximations, the vorticity interaction, and the shock-wave heating effect are unimportant in this case. For the present experiments, the effects of transport processes at the shock wave are numerically small in comparison with surface slip for the sharp flat plate at zero angle of attack, and it is postulated that surface slip is the dominant low-density effect. The slip boundary conditions are discussed to demonstrate that there is a pressure jump at the surface, analogous to the classical velocity and temperature jump. This effect is evaluated using existing theories and is in qualitative agreement with the experimental data. The slip boundary conditions are examined in light of the present experiments at zero angle of attack, and it is shown that the usual firstorder boundary conditions are inapplicable for the case of a cold wall.
Author : V. N. Gusev
Publisher :
ISBN 13 :
Total Pages : 16 pages
Book Rating : 4.:/5 (227 download)
Download or read book Experimental Study of Heat Transfer in a Critical Point of Sphere in Hypersonic Low-Density Flow written by V. N. Gusev and published by . This book was released on 1975 with total page 16 pages. Available in PDF, EPUB and Kindle. Book excerpt: In an experimental study of heat transfer at the critical point of a sphere the possibility is confirmed of using underexpanded nozzles in hypersonic wind tunnels for radiation of the flow about the models over a wide range of Reynolds numbers. Experiments were carried out in a hypersonic shock tube with numbers M
Author : United States. Congress. House. Committee on Science and Astronautics
Publisher :
ISBN 13 :
Total Pages : 854 pages
Book Rating : 4.:/5 (319 download)
Download or read book 1972 NASA Authorization written by United States. Congress. House. Committee on Science and Astronautics and published by . This book was released on 1971 with total page 854 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 592 pages
Book Rating : 4.F/5 ( download)
Download or read book Air Force Research Resumés written by and published by . This book was released on with total page 592 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :
Publisher :
ISBN 13 :
Total Pages : 892 pages
Book Rating : 4.:/5 (31 download)
Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1994 with total page 892 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Surendra P. Sharma
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book NASA Ames's Electric Arc-driven Shock Tube Facility and Research on Nonequilibrium Phenomena in Low Density Hypersonic Flows written by Surendra P. Sharma and published by . This book was released on 1992 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author : Aeronautical Research Council. Hypersonics Sub-Committee
Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)
Download or read book Current U.K. Research on Hypersonic Laminar Boundary Layers Including Shock Interaction, Separation and Low-density Flows written by Aeronautical Research Council. Hypersonics Sub-Committee and published by . This book was released on 1966 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:
