The Laminar Boundary Layer Equations
Title | The Laminar Boundary Layer Equations PDF eBook |
Author | N. Curle |
Publisher | Courier Dover Publications |
Pages | 177 |
Release | 2017-03-17 |
Genre | Science |
ISBN | 0486812391 |
Thorough introduction to boundary layer problems offers an ordered, logical presentation accessible to undergraduates. The text's careful expositions of the limitations and accuracy of various methods will also benefit professionals. 1962 edition.
The Laminar Boundary Layer Equations
Title | The Laminar Boundary Layer Equations PDF eBook |
Author | N. Curle |
Publisher | |
Pages | 162 |
Release | 1962 |
Genre | Boundary layer |
ISBN |
The Solution of the Laminar-boundary-layer Equation for the Flat Plate for Velocity and Temperature Fields for Variable Physical Properties and for the Diffusion Field at High Concentration
Title | The Solution of the Laminar-boundary-layer Equation for the Flat Plate for Velocity and Temperature Fields for Variable Physical Properties and for the Diffusion Field at High Concentration PDF eBook |
Author | H. Shuh |
Publisher | |
Pages | 28 |
Release | 1950 |
Genre | Boundary layer |
ISBN |
In connection with Pohlhausen's solution for the temperature field on the flat plate, a series of formulas were indicated by means of which the velocity and temperature field for variable physical characteristics can be computed by an integral equation and an iteration method based on it. With it, the following cases were solved: On the assumption that the viscosity simply varies with the temperature while the other fluid properties remain constant, the velocity and temperature field on the heated and cooled plate, respectively, was computed at the Prandtl numbers 12.5 and 100 (viscous fluids). A closer study of these two cases resulted in general relations: The calculations for a gas of Pr number 0.7 (air) were conducted on the assumption that all fluid properties vary with the temperature, and the velocities are low enough for the heat of friction to be discounted. The result was a thickening of the boundary layers, but no appreciable modification in shearing stress or heat-transfer coefficient.
Boundary-Layer Theory
Title | Boundary-Layer Theory PDF eBook |
Author | Hermann Schlichting (Deceased) |
Publisher | Springer |
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.
Boundary Layers
Title | Boundary Layers PDF eBook |
Author | Alec David Young |
Publisher | AIAA (American Institute of Aeronautics & Astronautics) |
Pages | 296 |
Release | 1989 |
Genre | Science |
ISBN |
Following an introduction to the basic physical concepts and the theoretical framework of boundary layers, discussion includes laminar boundary layers, the physics of the transition from laminar to turbulent flow, the turbulent boundary layer and its governing equations in time-averaging form, drag prediction by integral methods, turbulence modeling and differential methods, and current topics and problems in research and industry.
The laminar boundary layer equations
Title | The laminar boundary layer equations PDF eBook |
Author | |
Publisher | |
Pages | |
Release | 1962 |
Genre | |
ISBN |
Boundary-layer Similar Solutions and Correlation Equations for Laminar Heat-transfer Distribution in Equilibrium Air at Velocities Up to 41,100 Feet Per Second
Title | Boundary-layer Similar Solutions and Correlation Equations for Laminar Heat-transfer Distribution in Equilibrium Air at Velocities Up to 41,100 Feet Per Second PDF eBook |
Author | Nathaniel B. Cohen |
Publisher | |
Pages | 72 |
Release | 1961 |
Genre | Aerodynamic heating |
ISBN |
Correlations of the transport property estimates of NASA TR R-50 are employed to determine locally similar solutions of the laminar boundary-layer equations for air in chemical equilibrium. Exact solutions for flat-plate flow, axisymmetric stagnation flow, and stagnation flow for yawed infinite cylinder are obtained, and a correlation formula for the heat-transfer distribution function for arbitrary favorable pressure gradient is determined. Extension to three-dimensional flows with small cross flow is briefly described.