Stability of separating subsonic boundary layers
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Stability of separating subsonic boundary layers

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Published by National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service [distributor in Hampton, Va, Springfield, VA .
Written in English


Book details:

Edition Notes

StatementJamal A. Masad, Ali H. Nayfeh.
SeriesNASA contractor report -- 4638., NASA contractor report -- NASA CR-4638.
ContributionsNayfeh, Ali Hasan, 1933-, Langley Research Center.
The Physical Object
FormatMicroform
Pagination1 v.
ID Numbers
Open LibraryOL17790640M
OCLC/WorldCa32801791

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Laminar boundary layers can be loosely classified according to their structure and the circumstances under which they are created. The thin shear layer which develops on an oscillating body is an example of a Stokes boundary layer, while the Blasius boundary layer refers to the well-known similarity solution near an attached flat plate held in an oncoming unidirectional flow and Falkner–Skan. The effect of a pressure gradient on the first mode of instability of compressible subsonic and supersonic boundary layers is investigated using linear stability theory. A pressure gradient is studied that generates potential‐flow Mach number distributions at the edge of the boundary layer of the form M e =cx n, where c is a constant and x is the dimensionless streamwise by: 4. Masad JA, Nayfeh AH () The influence of imperfections on the stability of subsonic boundary layers. In: Ashpis DE, Gatski TB, Hirsh R (eds) Instabilities and Turbulence in Engineering Flows. Kluwer Academic Publ., pp 65– CrossRef Google ScholarAuthor: A. V. Dovgal. The primary and subharmonic instabilities of separating compressible subsonic two-dimensional boundary layers in the presence of a two-dimensional roughness element on a flat plate are investigated.

Although zero-gradient boundary layers reduce the flutter region in the parameter space [15,16,18,19,[22][23][24][25], boundary layers over concave walls can be . @article{osti_, title = {A method for the direct numerical simulation of hypersonic boundary-layer instability with finite-rate chemistry}, author = {Marxen, Olaf, E-mail: @ and Aeronautics and Aerospace Department, von Karman Institute for Fluid Dynamics, Chaussée de Waterloo, 72, Rhode-St-Genèse and Magin, Thierry E. and Shaqfeh, Eric S.G. and Iaccarino. PAUL K. CHANG, in Separation of Flow, 1 Three-dimensional Laminar Flow Separation. The prediction of laminar separation for the arbitrary three-dimensional flow is complex due to crossflow. The available analyses for three-dimensional laminar flow are only approximate and are often based upon boundary layer theories. @article{osti_, title = {The Kelvin-Helmholtz instability of boundary-layer plasmas in the kinetic regime}, author = {Steinbusch, Benedikt, E-mail: [email protected] and Gibbon, Paul, E-mail: @ and Department of Mathematics, Centre for Mathematical Plasma Astrophysics, Katholieke Universiteit Leuven and Sydora, Richard D., E-mail: [email protected]

Fluid Mechanics, Second Edition deals with fluid mechanics, that is, the theory of the motion of liquids and gases. Topics covered range from ideal fluids and viscous fluids to turbulence, boundary layers, thermal conduction, and diffusion.   Supersonic separated and reattaching laminar flows. i - general theory and application to adiabatic boundary-layershock-wave interactions. Acceleration and cooling effects in laminar boundary layers - Subsonic, transonic, and supersonic speeds. L. H. BACK ; AIAA Journal Vol. 8, Cited by: American Institute of Aeronautics and Astronautics Sunrise Valley Drive, Suite Reston, VA Stability and separation of freely interacting boundary layers. Seventh International Conference on Numerical Methods in Fluid Dynamics, Separating, incompressible, laminar boundary-layer flow over a smooth step of small by: