A Review of High-speed, Convective, Heat-transfer Computation Methods
Author : Michael E. Tauber
Publisher :
Page : 44 pages
File Size : 50,87 MB
Release : 1989
Category : Aerodynamic heating
ISBN :
Author : Michael E. Tauber
Publisher :
Page : 44 pages
File Size : 50,87 MB
Release : 1989
Category : Aerodynamic heating
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 1052 pages
File Size : 11,31 MB
Release : 1956
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 544 pages
File Size : 34,54 MB
Release : 1962
Category : Outer space
ISBN :
A Chinese boy's greatest wish is to be an artist but he is too poor to buy a good brush until a wizard appears and gives him one with magic powers.
Author : BALLMAN
Publisher : Springer Science & Business Media
Page : 448 pages
File Size : 47,24 MB
Release : 2012-12-06
Category : 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 :
Publisher :
Page : 260 pages
File Size : 13,44 MB
Release : 1970
Category :
ISBN :
Author : John Paul Rowe
Publisher :
Page : 702 pages
File Size : 18,82 MB
Release : 1957
Category : Alloys
ISBN :
An investigation of overheating HS-31 alloy to temperatures of 1,650 degrees, 1,800 degrees, 1,900 degrees, and 2,000 degrees F during the course of rupture tests 1,500 degrees F was carried out. The overheating was applied periodically for 2 minutes in most of the tests. The intent was to develop basic information on the effect of overheats on creep- rapture properties in order to assist in the evaluation of damage from overheats during gas- turbine operation.
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 992 pages
File Size : 50,80 MB
Release : 1962
Category : Outer space
ISBN :
Author : Joseph G. Marvin
Publisher :
Page : 60 pages
File Size : 22,7 MB
Release : 1965
Category : Heat
ISBN :
Equilibrium convective heat transfer in several real gases was investigated. The gases considered were air, nitrogen, hydrogen, carbon dioxide, and argon. Solutions to the similar form of the boundary-layer equations were obtained for flight velocities to 30,000 ft/sec for a range of parameters sufficient to define the effects of pressure level, pressure gradient, boundary-layer-edge velocity, and wall temperature. Results are presented for stagnation-point heating and for the heating-rate distribution. For the range of parameters investigated the wall heat transfer depended on the transport properties near the wall and precise evaluation of properties in the high-energy portions of the boundary layer was not needed. A correlation of the solutions to the boundary-layer equations was obtained which depended only on the low temperature properties of the gases. This result can be used to evaluate the heat transfer in gases other than those considered. The largest stagnation-point heat transfer at a constant flight velocity was obtained for argon followed successively by carbon dioxide, air, nitrogen, and hydrogen. The blunt-body heating-rate distribution was found to depend mainly on the inviscid flow field. For each gas, correlation equations of boundary-layer thermodynamic and transport properties as a function of enthalpy are given for a wide range of pressures to a maximum enthalpy of 18,000 Btu/lb.
Author :
Publisher :
Page : 818 pages
File Size : 26,74 MB
Release : 1954
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 456 pages
File Size : 15,62 MB
Release : 1995
Category : Aeronautics
ISBN :
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.