An Entropy Correction Method for Unsteady Full Potential Flows with Strong Shocks
Author :
Publisher :
Page : 18 pages
File Size : 46,85 MB
Release : 1986
Category :
ISBN :
Author :
Publisher :
Page : 18 pages
File Size : 46,85 MB
Release : 1986
Category :
ISBN :
Author :
Publisher :
Page : 38 pages
File Size : 34,72 MB
Release : 1984
Category :
ISBN :
Author :
Publisher :
Page : 14 pages
File Size : 40,70 MB
Release : 1988
Category :
ISBN :
Author :
Publisher :
Page : 354 pages
File Size : 49,31 MB
Release : 1996
Category :
ISBN :
Four lifting-line methods were compared with flight test data from a research Puma helicopter and the accuracy assessed over a wide range of flight speeds. Hybrid CFD methods were also examined for two high-speed conditions. A parallel analytical effort was performed with the lifting-line methods to assess the effects of modeling assumptions and this provided insight into the adequacy of these methods for load predictions.
Author : Fathi Habashi
Publisher : CRC Press
Page : 932 pages
File Size : 44,61 MB
Release : 1995-11-22
Category : Technology & Engineering
ISBN : 9782884490320
First published in 1995. Routledge is an imprint of Taylor & Francis, an informa company.
Author : W. G. Habashi
Publisher :
Page : 968 pages
File Size : 41,65 MB
Release : 1985
Category : Mathematics
ISBN :
Author : Joseph L. Steger
Publisher :
Page : 102 pages
File Size : 11,26 MB
Release : 1984
Category : Airplanes
ISBN :
The goal of this research was to further develop zonal methods and three dimensional procedures for application of finite difference methods to solve complex aircraft configurations. For the task of three dimensional grid generation both elliptic and hyperbolic methods were developed. A chimera grid scheme, that is, the use of overset multiple grid systems, was also tested in two dimensions. In zonal methods several new algorithms were developed. These included combining transonic potential codes with thin layer Navier-Stokes equations, unsteady transonic potential, Euler and vector potential codes. This report summarizes the various numerical algorithms that were studied. (Author).
Author : TERRY L. HOLST
Publisher :
Page : 120 pages
File Size : 12,56 MB
Release : 1983
Category :
ISBN :
Author : J. B. Malone
Publisher :
Page : 166 pages
File Size : 42,48 MB
Release : 1984
Category : Aerodynamics, Transonic
ISBN :
This report describes a study performed to evaluate a 3D, full potential, computational method developed at the Lockheed-Georgia. This computational method was used to compute both steady and unsteady compressible flows about an F-5 fighter wing model. Comparisons are made between computed steady and unsteady aerodynamic data and available experimental data for the F-5 planform. Correlations are presented for steady, unsteady and quasi-steady surface pressure distributions and integrated loads coefficients. Originator-assigned keywords include: Computational fluid dynamics, Unsteady aerodynamics, and Transonic flow.
Author :
Publisher :
Page : 20 pages
File Size : 23,34 MB
Release : 1988
Category :
ISBN :