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Book ASME 66 WA FE 34

Download or read book ASME 66 WA FE 34 written by J. R. Shanebrook and published by . This book was released on 1966 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Small Cross flows in Three dimensional Laminar Boundary Layers with Suction Or Injection

Download or read book Small Cross flows in Three dimensional Laminar Boundary Layers with Suction Or Injection written by Y. Y. Chan and published by 1969.. This book was released on 1969 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: Three-dimensional laminar boundary layers with suction or injection are examined by using an approximate method based on a small cross-flow assumption. The basic equations are derived in detail and the computational method is developed. The method is tested against exact solutions and is found to be reasonably accurate. Two examples with the same external condition, but with different surface conditions, are analyzed. In one case the distribution of the normal velocity at the surface satisfies the similarity requirement and in the other case the normal velocity is constant over the complete surface. Although the results of these two cases are different in detail, the general trend of both shows that the three-dimensional behaviour of the boundary layer diminishes with suction and amplifies with injection. (Author).

Book Stability of Three dimensional Compressible Boundary Layers

Download or read book Stability of Three dimensional Compressible Boundary Layers written by Eli Reshotko and published by . This book was released on 1962 with total page 48 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A General Method for Calculating Three Dimensional Incompressible Laminar and Turbulent Boundary Layers  I  Swept Infinite Cylinders and Small Cross Flow

Download or read book A General Method for Calculating Three Dimensional Incompressible Laminar and Turbulent Boundary Layers I Swept Infinite Cylinders and Small Cross Flow written by and published by . This book was released on 1972 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents a general method for solving the laminar and turbulent boundary layer equations for swept infinite cylinders and for small cross flows. In the equations the Reynolds shear stress terms are eliminated by using an eddy viscosity concept. An efficient two-point finite-difference method used earlier by Keller and Cebeci for two dimensional flows is used to solve the governing equations. The method has been programmed on the IBM 370/165. (Author).

Book Applied Mechanics Reviews

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1974 with total page 628 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book NASA Technical Report

    Book Details:
  • Author : United States. National Aeronautics and Space Administration
  • Publisher :
  • Release : 1961
  • ISBN :
  • Pages : 774 pages

Download or read book NASA Technical Report written by United States. National Aeronautics and Space Administration and published by . This book was released on 1961 with total page 774 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Scientific and Technical Aerospace Reports

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 702 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Technical Abstract Bulletin

Download or read book Technical Abstract Bulletin written by Defense Documentation Center (U.S.) and published by . This book was released on 1967 with total page 784 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Aeronautical Report

    Book Details:
  • Author :
  • Publisher :
  • Release : 1969
  • ISBN :
  • Pages : 336 pages

Download or read book Aeronautical Report written by and published by . This book was released on 1969 with total page 336 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Method of Solving the Three dimensional Laminar Boundary layer Equations with Application to a Lifting Reentry Body

Download or read book A Method of Solving the Three dimensional Laminar Boundary layer Equations with Application to a Lifting Reentry Body written by Torstein K. Fannelop and published by . This book was released on 1966 with total page 165 pages. Available in PDF, EPUB and Kindle. Book excerpt: The general three-dimensional laminar compressible boundary-layer equations, written in terms of streamline coordinates, are reduced to a sequence of two-dimensional equations by means of a systematic perturbation procedure. The perturbation parameter is related to the inviscid streamline curvature and the lowest (zeroth-order) equations are identical with the small crossflow equations of Hayes. In addition, the equations for the first-order terms are given explicitly both in terms of physical and transformed (Lees-Levy) variables. Two alternate finite difference methods (for physical and transformed variables respectively) are developed to solve the zeroth as well as the first-order equations exactly. Local similarity methods are also considered for comparison. A variety of boundary conditions are possible including the case for which the heat and mass-transfer rates are coupled through an energy balance. The methods were applied to the problem of boundary-layer flow on a blunted cone at angle-of-attack. The results show that the crossflow often becomes rather large near the wall. The first-order corrections to the enthalpy and tangential velocity in the boundary layer are nevertheless small. (Author).

Book A General Method for Calculating Three dimensional Incompressible Laminar and Turbulent Boundary Layers

Download or read book A General Method for Calculating Three dimensional Incompressible Laminar and Turbulent Boundary Layers written by Tuncer Cebeci and published by . This book was released on 1972 with total page 63 pages. Available in PDF, EPUB and Kindle. Book excerpt: The report presents a general method for solving the laminar and turbulent boundary layer equations for swept infinite cylinders and for small cross flows. In the equations the Reynolds shear stress terms are eliminated by using an eddy viscosity concept. An efficient two-point finite-difference method used earlier by Keller and Cebeci for two dimensional flows is used to solve the governing equations. The method has been programmed on the IBM 370/165. (Author).