Accession Number:

ADP004055

Title:

Inviscid Compressible Flow Past a Multi-Element Aerofoil,

Descriptive Note:

Corporate Author:

UNIVERSITY OF MANCHESTER INST OF SCIENCE AND TECHNOLOGY (ENGLAND)

Personal Author(s):

Report Date:

1984-08-01

Pagination or Media Count:

15.0

Abstract:

A conformal transformation method is used to generate an orthogonal curvilinear grid for two- and three-element configurations. The compressible potential flow equations are solved by finite difference methods. The solution could serve as a starting point for an iterative solution of the full viscous compressible flow case. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE