Analysis of Laminar Boundary Layers on Right Circular Cones at Angle of Attack, Including Streamline-swallowing Effects
| Author | : Arloe Wesley Mayne (Jr.) |
| Publisher | : |
| Total Pages | : 114 |
| Release | : 1972 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
Analysis Of Laminar Boundary Layers On Right Circular Cones At Angle Of Attack Including Streamline Swallowing Effects
Download Analysis Of Laminar Boundary Layers On Right Circular Cones At Angle Of Attack Including Streamline Swallowing Effects full books in PDF, epub, and Kindle. Read online free Analysis Of Laminar Boundary Layers On Right Circular Cones At Angle Of Attack Including Streamline Swallowing Effects ebook anywhere anytime directly on your device. Fast Download speed and no annoying ads. We cannot guarantee that every ebooks is available!
Calculation of the Boundary-layer Flow in the Windward Symmetry Plane of a Spherically Blunted Axisymmetric Body at Angle of Attack, Including Streamline-swallowing Effects
| Author | : Arloe W. Mayne (Jr.) |
| Publisher | : |
| Total Pages | : 60 |
| Release | : 1973 |
| Genre | : Aerodynamics, Hypersonic |
| ISBN | : |
Three-dimensional compressible boundary-layer equations are particularized to the windward symmetry plane of a spherically blunted axisymmetric body at incidence under hypersonic conditions. Through the use eddy transport and streamwise intermittency both transitional and fully turbulent boundary layers may be treated. A scheme is presented for determining the outer-edge boundary conditions based on a mass flow balance treatment of the boundary-layer entrainment of the inviscid flow. A finite-difference technique is described for solving the set of partial differential equation governing the boundary-layer flow, and for treating the streamline-swallowing phenomenon.
Roll-damping Derivative Calculations for Spinning Sharp and Blunt Cones in Supersonic and Hypersonic Flow
| Author | : Arloe W. Mayne (Jr.) |
| Publisher | : |
| Total Pages | : 28 |
| Release | : 1979 |
| Genre | : Cone |
| ISBN | : |
The boundary-layer equations in a Crocco variables form have been numerically solved for flow over spinning sharp and blunt cones at zero incidence to supersonic and hypersonic streams. Both laminar and turbulent flows have been treated, and for the blunt cases swallowing of the inviscid entropy layer by the boundary layer has been considered. The item of primary interest is roll damping, and results of a parametric study involving Mach number, Reynolds number, cone angle, and bluntness ratio are presented. Limited comparisons with experimental data and another method of computation are also presented. (Author).
Computational Methods for Inviscid and Viscous Two-and-three-dimensional Flow Fields
| Author | : North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Fluid Dynamics Panel |
| Publisher | : |
| Total Pages | : 210 |
| Release | : 1975 |
| Genre | : Boundary value problems |
| ISBN | : |
Presents the recent developments in the numerical approach of fluid flow problems. Particular emphasis placed on numerical techniques for the solution of the compressible Navier-Stokes equations and the implementation of turbulence models, the computational techniques for boundary layers, hyperbolic partial differential equations, numerical stability of finite difference methods, numerical solutions of the Navier-Stokes equations for compressible fluids, and finite elements.--abs., report documentary page.
