A Weakly Nonlinear Theory for Wave-vortex Interactions in Curved Channel Flow
Author : Bart A. Singer
Publisher :
Page : 32 pages
File Size : 15,75 MB
Release : 1992
Category : Nonlinear theories
ISBN :
Author : Bart A. Singer
Publisher :
Page : 32 pages
File Size : 15,75 MB
Release : 1992
Category : Nonlinear theories
ISBN :
Author : P. Hall
Publisher :
Page : 44 pages
File Size : 50,51 MB
Release : 1987
Category : Fluid mechanics
ISBN :
Author : United States. National Aeronautics and Space Administration
Publisher :
Page : 318 pages
File Size : 14,81 MB
Release : 1991
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 28 pages
File Size : 35,62 MB
Release : 1992
Category : Science
ISBN :
Author : Institute for Computer Applications in Science and Engineering
Publisher :
Page : 40 pages
File Size : 48,91 MB
Release : 1988
Category :
ISBN :
Author : Bart A. Singer
Publisher :
Page : 32 pages
File Size : 31,30 MB
Release : 1992
Category :
ISBN :
Author : Peter W. Duck
Publisher : Springer Science & Business Media
Page : 458 pages
File Size : 18,30 MB
Release : 2012-12-06
Category : Science
ISBN : 9400917007
Most fluid flows of practical importance are fully three-dimensional, so the non-linear instability properties of three-dimensional flows are of particular interest. In some cases the three-dimensionality may have been caused by a finite amplitude disturbance whilst, more usually, the unperturbed state is three-dimensional. Practical applications where transition is thought to be associated with non-linearity in a three- dimensional flow arise, for example, in aerodynamics (swept wings, engine nacelles, etc.), turbines and aortic blood flow. Here inviscid `cross-flow' disturbances as well as Tollmien-Schlichting and Görtler vortices can all occur simultaneously and their mutual non-linear behaviour must be understood if transition is to be predicted. The non-linear interactions are so complex that usually fully numerical or combined asymptotic/numerical methods must be used. Moreover, in view of the complexity of the instability processes, there is also a growing need for detailed and accurate experimental information. Carefully conducted tests allow us to identify those elements of a particular problem which are dominant. This assists in both the formulation of a relevant theoretical problem and the subsequent physical validation of predictions. It should be noted that the demands made upon the skills of the experimentalist are high and that the tests can be extremely sophisticated - often making use of the latest developments in flow diagnostic techniques, automated high speed data gathering, data analysis, fast processing and presentation.
Author : M.Y. Hussaini
Publisher : Springer Science & Business Media
Page : 509 pages
File Size : 15,87 MB
Release : 2012-12-06
Category : Science
ISBN : 1461234328
The ability to predict and control viscous flow phenomena is becoming increasingly important in modern industrial application. The Instability and Transition Workshop at Langley was extremely important in help§ ing the scientists community to access the state of knowledge in the area of transition from laminar to turbulent flow, to identify promising future areas of research and to build future interactions between researchers worldwide working in the areas of theoretical, experimental and computational fluid and aero dynamics. The set of two volume contains panel discussions and research contribution with the following objectives: (1) expose the academic community to current technologically important issues of instability and transitions in shear flows over the entire speed range, (2) acquaint the academic community with the unique combination of theoretical, computational and experimental capabilities at LaRC and foster interaction with these facilities. (3) review current state-of-the-art and propose future directions for instability and transition research, (4) accelerate progress in elucidating basic understanding of transition phenomena and in transferring this knowledge into improved design methodologies through improved transition modeling, and (5) establish mechanism for continued interaction.
Author :
Publisher :
Page : 944 pages
File Size : 32,7 MB
Release : 1995-11
Category : Government publications
ISBN :
Author :
Publisher :
Page : 1224 pages
File Size : 34,65 MB
Release :
Category : Government publications
ISBN :