Accession Number:

AD0763283

Title:

Shock Wave Incidence on a Wedge Moving at Supersonic Speed,

Descriptive Note:

Corporate Author:

FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s):

Report Date:

1973-06-06

Pagination or Media Count:

12.0

Abstract:

A flow which is developing at the upper surface of a wedge moving at supersonic speed, when a plane shock wave is incident on the wedge, can be calculated in the framework of a linearized theory, if the point which is determined by two parameters of the wedge belongs to a certain area in the reference plane.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE