Book Description
Advances in Applied Mechanics
Author :
Publisher : Academic Press
Page : 303 pages
File Size : 17,50 MB
Release : 1948-01-01
Category : Technology & Engineering
ISBN : 0080575544
Advances in Applied Mechanics
Author : Chia-Chʻiao Lin
Publisher : World Scientific
Page : 1048 pages
File Size : 43,31 MB
Release : 1987-01-01
Category : Astrophysics
ISBN : 9789971503185
Author : Lester Lees
Publisher :
Page : 176 pages
File Size : 27,31 MB
Release : 1946
Category : Laminar boundary layer
ISBN :
Report is presented in two parts: Part 1 deals with the general mathematical theory; Part 2 deals with the limiting case of infinite Reynolds numbers.
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 986 pages
File Size : 20,22 MB
Release : 1958
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 900 pages
File Size : 11,12 MB
Release : 1957
Category : Aeronautics
ISBN :
Author : United States. National Advisory Committee for Aeronautics
Publisher :
Page : 40 pages
File Size : 30,89 MB
Release : 1957
Category : Aeronautics
ISBN :
Author :
Publisher :
Page : 512 pages
File Size : 41,68 MB
Release : 1962
Category :
ISBN :
Author : Tuncer Cebeci
Publisher : Springer
Page : 502 pages
File Size : 48,75 MB
Release : 2009-09-02
Category : Science
ISBN : 9783540807315
This second edition of the book, Modeling and Computation of Boundary-Layer Flows^ extends the topic to include compressible flows. This implies the inclusion of the energy equation and non-constant fluid properties in the continuity and momentum equations. The necessary additions are included in new chapters, leaving the first nine chapters to serve as an introduction to incompressible flows and, therefore, as a platform for the extension. This part of the book can be used for a one semester course as described below. Improvements to the incompressible flows portion of the book include the removal of listings of computer programs and their description, and their incor poration in two CD-ROMs. A listing of the topics incorporated in the CD-ROM is provided before the index. In Chapter 7 there is a more extended discussion of initial conditions for three-dimensional flows, application of the characteristic box to a model problem and discussion of flow separation in three-dimensional laminar flows. There are also changes to Chapter 8, which now includes new sections on Tollmien-Schlichting and cross-flow instabilities and on the predic tion of transition with parabolised stability equations, and Chapter 9 provides a description of the rational behind interactive boundary-layer procedures.
Author : Hermann Schlichting (Deceased)
Publisher : Springer
Page : 814 pages
File Size : 21,25 MB
Release : 2016-10-04
Category : 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 : Alvin Seiff
Publisher :
Page : 654 pages
File Size : 39,19 MB
Release : 1954
Category : Aerodynamics, Supersonic
ISBN :
Heat-transfer data from four wind-tunnel experiments and two free-flight experiments with turbulent boundary layers have been examined to see whether or not they are well represented by the Reynolds analogy or a modification thereof. The heat-transfer results are put into the form of dimensionless Stanton numbers based on fluid properties at the outer edge of the boundary layer and are compared with skin-friction coefficients for the same Mach numbers and wall to free-stream temperature ratios as obtained from an interpolation of the existing skin-friction data. The effective Reynolds number is taken to be the length Reynolds number measured from the effective turbulent origin, a position which differs importantly from the leading edge of the test surface in some cases.