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.
Descriptors:
Subject Categories:
- Fluid Mechanics