Scientific and Technical Aerospace Reports
Author :
Publisher :
Page : 564 pages
File Size : 34,13 MB
Release : 1992
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 564 pages
File Size : 34,13 MB
Release : 1992
Category : Aeronautics
ISBN :
Author : Ernst Heinrich Hirschel
Publisher : Springer Science & Business Media
Page : 396 pages
File Size : 20,22 MB
Release : 2013-10-29
Category : Technology & Engineering
ISBN : 3642413781
Viscous flow is treated usually in the frame of boundary-layer theory and as two-dimensional flow. Books on boundary layers give at most the describing equations for three-dimensional boundary layers, and solutions often only for some special cases. This book provides basic principles and theoretical foundations regarding three-dimensional attached viscous flow. Emphasis is put on general three-dimensional attached viscous flows and not on three-dimensional boundary layers. This wider scope is necessary in view of the theoretical and practical problems to be mastered in practice. The topics are weak, strong, and global interaction, the locality principle, properties of three-dimensional viscous flow, thermal surface effects, characteristic properties, wall compatibility conditions, connections between inviscid and viscous flow, flow topology, quasi-one- and two-dimensional flows, laminar-turbulent transition and turbulence. Though the primary flight speed range is that of civil air transport vehicles, flows past other flying vehicles up to hypersonic speeds are also considered. Emphasis is put on general three-dimensional attached viscous flows and not on three-dimensional boundary layers, as this wider scope is necessary in view of the theoretical and practical problems that have to be overcome in practice. The specific topics covered include weak, strong, and global interaction; the locality principle; properties of three-dimensional viscous flows; thermal surface effects; characteristic properties; wall compatibility conditions; connections between inviscid and viscous flows; flow topology; quasi-one- and two-dimensional flows; laminar-turbulent transition; and turbulence. Detailed discussions of examples illustrate these topics and the relevant phenomena encountered in three-dimensional viscous flows. The full governing equations, reference-temperature relations for qualitative considerations and estimations of flow properties, and coordinates for fuselages and wings are also provided. Sample problems with solutions allow readers to test their understanding.
Author : National Research Council Canada
Publisher :
Page : 570 pages
File Size : 29,1 MB
Release : 1968
Category : Aeronautics
ISBN :
Author : Spencer Sherwin
Publisher : Springer Nature
Page : 809 pages
File Size : 19,54 MB
Release : 2021-07-30
Category : Computers
ISBN : 3030679020
This volume comprises the carefully revised papers of the 9th IUTAM Symposium on Laminar-Turbulent Transition, held at the Imperial College, London, UK, in September 2019. The papers focus on the leading research in understanding transition to turbulence, which is a challenging topic of fluid mechanics and arises in many modern technologies as well as in nature. The proceedings are of interest for researchers in fluid mechanics and industry who have to handle these types of problems, such as in the aeronautical sector.
Author :
Publisher :
Page : 620 pages
File Size : 28,34 MB
Release : 1974
Category : Mechanics, Applied
ISBN :
Author :
Publisher :
Page : 784 pages
File Size : 21,95 MB
Release : 1969-10
Category : Science
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 588 pages
File Size : 30,68 MB
Release : 1962
Category : Aeronautics
ISBN :
Author : National Aeronautics and Space Administration
Publisher : CreateSpace
Page : 86 pages
File Size : 35,94 MB
Release : 2013-11
Category : History
ISBN : 9781493794324
Laminar-flow control is an area of aeronautical research that has a long history at NASA's Langley Research Center, Dryden Flight Research Center, their predecessor organizations, and elsewhere. In this monograph, Albert L. Braslow, who spent much of his career at Langley working with this research, presents a history of that portion of laminar-flow technology known as active laminar-flow control, which employs suction of a small quantity of air through airplane surfaces. This important technique offers the potential for significant reduction in drag and, thereby, for large increases in range or reductions in fuel usage for aircraft. For transport aircraft, the reductions in fuel consumed as a result of laminar-flow control may equal 30 percent of present consumption. Given such potential, it is obvious that active laminar-flow control with suction is an important technology. In this study, the author covers the early history of the subject and brings the story all the way to the mid-1990s with an emphasis on flight research, much of which occurred at Dryden.
Author : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher :
Page : 242 pages
File Size : 11,31 MB
Release : 1982
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 1306 pages
File Size : 15,45 MB
Release : 1969
Category : Nuclear science abstracts
ISBN :