The Gortler Vortex Instability Mechanism In Three Dimensional Boundary Layers
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The Goertler Vortex Instability Mechanism in Three-dimensional Boundary Layers
Author | : Institute for Computer Applications in Science and Engineering |
Publisher | : |
Total Pages | : 44 |
Release | : 1984 |
Genre | : |
ISBN | : |
IUTAM Symposium on Nonlinear Instability and Transition in Three-Dimensional Boundary Layers
Author | : Peter W. Duck |
Publisher | : Springer Science & Business Media |
Total Pages | : 458 |
Release | : 2012-12-06 |
Genre | : 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.
Vortex Instabilities in 3D Boundary Layers: The Relationship Between Goertler and Crossflow Vortices
Author | : Institute for Computer Applications in Science and Engineering |
Publisher | : |
Total Pages | : 82 |
Release | : 1990 |
Genre | : |
ISBN | : |
On the Stability of Nonlinear Viscous Vortices in Three-dimensional Boundary Layers
Author | : Institute for Computer Applications in Science and Engineering |
Publisher | : |
Total Pages | : 56 |
Release | : 1992 |
Genre | : |
ISBN | : |
Perspectives in Turbulence Studies
Author | : Hans U. Meier |
Publisher | : Springer Science & Business Media |
Total Pages | : 512 |
Release | : 2012-12-06 |
Genre | : Science |
ISBN | : 3642829945 |
The present volume entitled "Perspectives in Turbulence Stud ies" is dedicated to Dr. Ing. E. h. Julius C. Rotta in honour of his 75th birthday. J. C. Rotta, born on January 1, 1912, started his outstanding career in an unusual way, namely in a drawing office (1928 - 1931). At the same time he - as a purely self taught perso- took a correspondence course in airplane construction. From 1934 to 1945 he worked in the aircraft industry on different subjects in the fields of flight mechanics, structures, air craft design, and aerodynamics. In 1945 he moved to Gottingen and worked from that time at the Aerodynamische Versuchsanstalt (AVA, now DFVLR) and the Max-Planck-Institut fur Stromungsforschung (1947-1958), interrupted only by a stay in the U. S. at the Glenn L. Martin Company (1954 - 1955) and a visiting professorship at the Laval University in Quebec, Canada (1956). Already during his activities in industry, Dr. Rotta discovered his special liking for aerodynamics. In Gottingen, he was attracted by Ludwig Prandtl's discussions about problems associated with turbulence and in particular his new contribution to fully developed turbulence, published in 1945. At that time, W. Heisenberg and C. F. v. Weizacker pub lished their results on the energy spectra of isotropic turbu lence at large wave numbers. Since that time his main research interest in reasearch has been in turbulence problems.
Goertler Vortices in Growing Boundary Layers: The Leading Edge Receptivity Problem, Linear Growth and the Nonlinear Breakdown Stage
Author | : Institute for Computer Applications in Science and Engineering |
Publisher | : |
Total Pages | : 80 |
Release | : 1989 |
Genre | : Aerodynamics |
ISBN | : |
Transition, Turbulence and Combustion
Author | : M.Y. Hussaini |
Publisher | : Springer Science & Business Media |
Total Pages | : 394 |
Release | : 2012-12-06 |
Genre | : Science |
ISBN | : 9401110328 |
These two volumes contain the proceedings of the Workshop on Transition, Turbulence and Combustion, sponsored by the Insti tute for Computer Applications in Science and Engineering (ICASE) and the NASA Langley Research Center (LaRC), during June 7 to July 2, 1993. Volume I contains the contributions from the transi tion research, and Volume II contains the contributions from both the turbulence and combustion research. This is the third workshop in the series on the subject. The first was held in 1989, the second in 1991, and their proceedings were published by Springer-Verlag under the titles "Instability and Transition" (edited by M. Y. Hussaini and R. G. Voigt) and "Instability, Transition and Turbulence" (edited by M. Y. Hussaini, A. Kumar and C. L. Streett) respectively. The objectives of these workshops are to expose the academic community to current technologically important issues of transition, turbulence and combustion, and to acquaint the academic commu nity with the unique combination of theoretical, computational and experimental capabilities at LaRC. It is hoped these will foster con tinued interactions, and accelerate progress in elucidating the funda mental phenomena of transition, turbulence and combustion. The research areas of interest in transition covered the full range of the subject: linear and nonlinear stability, direct and large-eddy simulation and phenomenological modeling of the transition zone.