A Comparison of Two Integral Equation Methods for High Subsonic Lifting Flows

1 February 1975

journal article
research article
Published by Cambridge University Press (CUP) in Aeronautical Quarterly

Vol. 26 (1) , 56-58
https://doi.org/10.1017/s0001925900007198

Abstract

Summary A comparison is made of two recently published integral equation methods for calculating the high subsonic flow around lifting and non-lifting aerofoils. It is shown that one method leads to a non-unique solution.

Keywords

MADE
SUMMARY
AEROFOILS
PUBLISHED
INTEGRAL EQUATION METHODS
COMPARISON
SUBSONIC

This publication has 1 reference indexed in Scilit:

The Transonic Aerofoil Problem with Embedded Shocks
Aeronautical Quarterly, 1973