Author: Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 702
Book Description
Convective and Radiative Heat Transfer to Blunt Bodies at Angle of Attack, Part II Final Report
Author: NACA Conference on Aircraft Loads, Structures, and Flutter
Author: Super- and Hypersonic Aerodynamics and Heat Transfer
Author: V.Z. PartonPublisher: Routledge
ISBN: 1351412949
Category : Technology & Engineering
Languages : en
Pages : 352
Book Description
Recent government and commercial efforts to develop orbital and suborbital passenger and transport aircraft have resulted in a burgeoning of new research. The articles in this book, translated from Russian, were contributed by the world's leading authorities on supersonic and hypersonic flows and heat transfer. This superb book addresses the physics and engineering aspects of ultra high-speed aerodynamic problems. Thorough coverage is given to an array of specific problem-solving equations. Super- and Hypersonic Aerodynamics and Heat Transfer will be essential reading for all aeronautical engineers, mechanical engineers, mathematicians, and physicists involved in this exciting field of research.
NASA Technical Note
Author: Pressure and Laminar Heat Transfer Results in Three-dimensional Hypersonic Flow
Author: Victor ZakkayPublisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 66
Book Description
Convective Heat-transfer Rates on Large-scale Conical Bodies at Hypersonic Speeds
Author: David Alexander StewartPublisher:
ISBN:
Category : Aerodynamic heating
Languages : en
Pages : 28
Book Description
Heat-transfer rates were measured on large-angle conical bodies with large half-angles between 50 degrees and 90 degrees, at angles of attack from 0 degrees. The results at 0 degree angle of attack were predicted with Lees' similarity theory, using calculated flow properties at the boundary-layer edge. The calculated flow properties were obtained from Newtonian theory for the 50 degree cone and from a one- or two-strip solution using the method of integral relations for other cones. At 0 degree angle of attack, an increase in cone angle resulted in a decrease in the heating rate over much of the body. However, high heating rates occurred at the shoulder of the both the half-angle = 80 degree and half-angle =90 degree shapes because of local pressure gradients. On the windward side of the cones, the heating rate increased with angle of attack.
Convective Heat Transfer to a Lifting Flat-faced-cone Entry Body
Author: James E. TerryPublisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 46
Book Description
U.S. Government Research Reports
Author: Scientific and Technical Aerospace Reports
Author: Monthly Catalog of United States Government Publications
Author: United States. Superintendent of DocumentsPublisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1248
Book Description