Accession Number:

AD0775108

Title:

On the Solution to the Problem of the Flow around a V-Shaped Wing with an Intense Shock Wave on the Leading Edge,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1974-02-01

Pagination or Media Count:

14.0

Abstract:

A report is made on the effect of initial and boundary conditions on the numerical solution to the problem of the flow around a V-shaped wing with supersonic leading edges.

Subject Categories:

  • Aerodynamics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE