Accession Number : AD0819359

Title :   LAMINAR HEAT TRANSFER TO A SWEPT LEADING EDGE IN HYPERSONIC FLOW.

Descriptive Note : Final rept. Jun 65-Mar 66,

Corporate Author : NORTH AMERICAN AVIATION INC COLUMBUS OH COLUMBUS DIV

Personal Author(s) : Fong, Michael C. ; Freeman, Clifford G.

Report Date : APR 1967

Pagination or Media Count : 215

Descriptors :   (*SWEPTBACK WINGS, AERODYNAMIC HEATING), (*HEAT TRANSFER, LEADING EDGES), HYPERSONIC CHARACTERISTICS, LAMINAR FLOW, BLUNT BODIES, TURBULENT BOUNDARY LAYER, THREE DIMENSIONAL FLOW, COMPRESSIBLE FLOW, ANGLE OF ATTACK, PERTURBATION THEORY, FLOW FIELDS, EQUATIONS OF STATE, DIFFERENTIAL EQUATIONS, CYLINDRICAL BODIES, YAW, THEORY, PRESSURE, NUMERICAL METHODS AND PROCEDURES, PRANDTL NUMBER, COMPUTER PROGRAMS.

Subject Categories : Fluid Mechanics
      Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE