Accession Number:

AD0256180

Title:

PRELIMINARY REPORT ON THE FIN-WING INTERACTION PROBLEM

Descriptive Note:

Technical rept.,

Corporate Author:

GENERAL APPLIED SCIENCE LABS INC HEMPSTEAD N Y

Personal Author(s):

Report Date:

1960-07-01

Pagination or Media Count:

1.0

Abstract:

An idealization of the shock wave boundary layer interaction problem which arises when a fin is installed on a wing or planar surface is described. It is shown that a reasonable first step in the analysis of this interaction is the two-dimensional interaction of an oblique shock wave on a laminar boundary layer. In view of recent developments in boundary layer theory an analysis of this problem seems possible. Accordingly a flow model and method of analysis are outlined and the next steps in the investigation described.

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE