Accession Number:

AD0677094

Title:

FLOW AROUND A CORNER FOR AIR IN EQUILIBRIUM (PRANDTL-MEYER EXPANSION),

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CALIF

Personal Author(s):

Report Date:

1960-10-27

Pagination or Media Count:

40.0

Abstract:

The document contains a theoretical treatment of the supersonic flow of air around a corner, using the assumptions made by Prandtl and develped by Meyer.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE