A series of numerical experiments are described which solve for the time dependent flow field around a circular cylinder accelerated to supersonic speeds. The study is performed using a computer program developed by Scala and Gordon which models the full time-dependent Navier-Stokes equations. Results are presented for Mach two flow past a cylinder at freestream Reynolds numbers of 15.0, 46.8, 157.2, and 704.6, based on cylinder diameter. The numerical results are compared with analytical solutions and experimental measurements and the accuracy of the numerical results is discussed. These comparisons show where the author's numerical solutions of the Navier-Stokes equations fail to give accurate results."April 1972."Includes bibliographic r...
A numerical study of the steady, two-dimensional incompressible flow past a cascade of circular cyli...
In the present paper; an experimental and numerical investigations of drag reduction on a grooved ci...
The paper describes the results obtained from a multigrid accelerated Navier-Stokes solver. The meth...
A numerical model is developed on a Discrete Fourier Transform-finite difference algorithm to determ...
A theoretical and experimental study has been conducted of a flow field about a hemisphere-cylinder ...
Numerical solutions of the Navier-Stokes equations were obtained for separated flows around a circul...
This work is part of a cooperative research, development, test and evaluation program that brings sc...
A numerical study of the aerodynamics of a circular cylinder section in proximity to the ground surf...
A computer code for solving the two-dimensional compressible Navier-Stokes equations governing the s...
The effect of the spanwise extension of the solution domain on the three-dimensional wake of a circu...
The flowfield in the wake of circular cylinders was studies experimentally at a Mach number of 6 to ...
A numerical method for a finite difference approach has been established for the analysis and contro...
This document reports on the computation of Ramjet Internal Flowfields. It is divided into two secti...
The goal of this project is to numerically solve the Navier-Stokes equations by using different nume...
In this thesis, a numerical algorithm based on the integro-differential method is presented to study...
A numerical study of the steady, two-dimensional incompressible flow past a cascade of circular cyli...
In the present paper; an experimental and numerical investigations of drag reduction on a grooved ci...
The paper describes the results obtained from a multigrid accelerated Navier-Stokes solver. The meth...
A numerical model is developed on a Discrete Fourier Transform-finite difference algorithm to determ...
A theoretical and experimental study has been conducted of a flow field about a hemisphere-cylinder ...
Numerical solutions of the Navier-Stokes equations were obtained for separated flows around a circul...
This work is part of a cooperative research, development, test and evaluation program that brings sc...
A numerical study of the aerodynamics of a circular cylinder section in proximity to the ground surf...
A computer code for solving the two-dimensional compressible Navier-Stokes equations governing the s...
The effect of the spanwise extension of the solution domain on the three-dimensional wake of a circu...
The flowfield in the wake of circular cylinders was studies experimentally at a Mach number of 6 to ...
A numerical method for a finite difference approach has been established for the analysis and contro...
This document reports on the computation of Ramjet Internal Flowfields. It is divided into two secti...
The goal of this project is to numerically solve the Navier-Stokes equations by using different nume...
In this thesis, a numerical algorithm based on the integro-differential method is presented to study...
A numerical study of the steady, two-dimensional incompressible flow past a cascade of circular cyli...
In the present paper; an experimental and numerical investigations of drag reduction on a grooved ci...
The paper describes the results obtained from a multigrid accelerated Navier-Stokes solver. The meth...