Boundary-layer Stability Theory
Author | : Leslie M. Mack |
Publisher | : |
Total Pages | : 406 |
Release | : 1969 |
Genre | : Boundary layer |
ISBN | : |
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Author | : Leslie M. Mack |
Publisher | : |
Total Pages | : 406 |
Release | : 1969 |
Genre | : Boundary layer |
ISBN | : |
Author | : L. M. Mack |
Publisher | : |
Total Pages | : 82 |
Release | : 1984 |
Genre | : |
ISBN | : |
Partial contents: Historical Background; Elements of Stability Theory; Incompressible Stability Theory; Incompressible Inviscid Theory; Numerical Techniques; Viscous Instability; Numerical Results - 2 D boundary layers; Harmonic Point Sources of Instability Waves; Compressible Stability Theory; Compressible Inviscid Theory; Compressible Viscous Theory; Forcing Theory; Three Dimensional Boundary Layers; Rotating Disk--A prototype 3D boundary layer; Falkner-Skan-Cooke Boundary Layers; Transonic Infinite-Span Swept Wing Boundary Layer; and Coefficient Matrix of Compressible Stability Equations.
Author | : Peter Chiarulli |
Publisher | : |
Total Pages | : 230 |
Release | : 1948 |
Genre | : Aerodynamics |
ISBN | : |
Author | : National Aeronautics and Space Administration (NASA) |
Publisher | : Createspace Independent Publishing Platform |
Total Pages | : 24 |
Release | : 2018-08-20 |
Genre | : |
ISBN | : 9781722341183 |
The viewgraphs and discussion of linear stability theory and three dimensional boundary layer transition are provided. The ability to predict, using analytical tools, the location of boundary layer transition over aircraft-type configurations is of great importance to designers interested in laminar flow control (LFC). The e(sup N) method has proven to be fairly effective in predicting, in a consistent manner, the location of the onset of transition for simple geometries in low disturbance environments. This method provides a correlation between the most amplified single normal mode and the experimental location of the onset of transition. Studies indicate that values of N between 8 and 10 correlate well with the onset of transition. For most previous calculations, the mean flows were restricted to two-dimensional or axisymmetric cases, or have employed simple three-dimensional mean flows (e.g., rotating disk, infinite swept wing, or tapered swept wing with straight isobars). Unfortunately, for flows over general wing configurations, and for nearly all flows over fuselage-type bodies at incidence, the analysis of fully three-dimensional flow fields is required. Results obtained for the linear stability of fully three-dimensional boundary layers formed over both wing and fuselage-type geometries, and for both high and low speed flows are discussed. When possible, transition estimates form the e(sup N) method are compared to experimentally determined locations. The stability calculations are made using a modified version of the linear stability code COSAL. Mean flows were computed using both Navier Stokes and boundary-layer codes. Spall, Robert E. and Malik, Mujeeb R. Unspecified Center ...
Author | : Rand Corporation |
Publisher | : |
Total Pages | : 35 |
Release | : 1975 |
Genre | : |
ISBN | : |
Author | : Hermann Schlichting (Deceased) |
Publisher | : Springer |
Total Pages | : 814 |
Release | : 2016-10-04 |
Genre | : Technology & Engineering |
ISBN | : 366252919X |
This new edition of the near-legendary textbook by Schlichting and revised by Gersten presents a comprehensive overview of boundary-layer theory and its application to all areas of fluid mechanics, with particular emphasis on the flow past bodies (e.g. aircraft aerodynamics). The new edition features an updated reference list and over 100 additional changes throughout the book, reflecting the latest advances on the subject.
Author | : D.L. Dwoyer |
Publisher | : Springer Science & Business Media |
Total Pages | : 361 |
Release | : 2013-03-09 |
Genre | : Science |
ISBN | : 1461247241 |
This volume is the collection of papers presented at the workshop on 'The Stability of Spatially Varying and Time Dependent Flows" sponsored by the Institute for Computer Applications in Science and Engineering (lCASE) and NASA Langley Research Center (LaRC) during August 19- 23, 1985. The purpose of this workshop was to bring together some of the experts in the field for an exchange of ideas to update the current status of knowledge and to help identify trends for future research. Among the invited speakers were D.M. Bushnell, M. Goldstein, P. Hall, Th. Herbert, R.E. Kelly, L. Mack, A.H. Nayfeh, F.T. Smith, and C. von Kerczek. The contributed papers were by A. Bayliss, R. Bodonyi, S. Cowley, C. Grosch, S. Lekoudis, P. Monkewitz, A. Patera, and C. Streett. In the first article, Bushnell provides a historical background on laminar flow control (LFC) research and summarizes the crucial role played by stability theory in LFC system design. He also identifies problem areas in stability theory requiring further research from the view-point of ap plications to LFC design. It is an excellent article for theoreticians looking for some down-to-earth applications of stability theory.
Author | : Herrmann Schlichting |
Publisher | : Springer Science & Business Media |
Total Pages | : 840 |
Release | : 2003-05-20 |
Genre | : Technology & Engineering |
ISBN | : 9783540662709 |
A new edition of the almost legendary textbook by Schlichting completely revised by Klaus Gersten is now available. This book presents a comprehensive overview of boundary-layer theory and its application to all areas of fluid mechanics, with emphasis on the flow past bodies (e.g. aircraft aerodynamics). It contains the latest knowledge of the subject based on a thorough review of the literature over the past 15 years. Yet again, it will be an indispensable source of inexhaustible information for students of fluid mechanics and engineers alike.