Shock Wave Incidence on a Wedge Moving at Supersonic Speed,
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.
Document Details
- Document Type
- Technical Report
- Publication Date
- Jun 06, 1973
- Accession Number
- AD0763283
Entities
People
- G. M. Arutyunyan
Organizations
- National Air and Space Intelligence Center