Accession Number : AD0677094

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

Corporate Author : GENERAL DYNAMICS/ASTRONAUTICS SAN DIEGO CALIF

Personal Author(s) : D'Attorre,L.

Report Date : 27 OCT 1960

Pagination or Media Count : 40

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.

Descriptors :   (*TWO DIMENSIONAL FLOW, SUPERSONIC CHARACTERISTICS), AIR, EQUILIBRIUM(PHYSIOLOGY), MATHEMATICAL ANALYSIS, EQUATIONS OF MOTION, ENTHALPY, PRESSURE, DENSITY, DEFLECTION, COMPUTER PROGRAMMING, WALLS, TEMPERATURE, EQUATIONS OF STATE

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE