Accession Number : AD0653181

Title :   SIMILARITY SOLUTIONS FOR THE RETARDED COMPRESSIBLE BOUNDARY LAYER WITH HEAT AND MASS TRANSFER,

Corporate Author : AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Ball,Karlheinz O. W.

Report Date : MAR 1967

Pagination or Media Count : 22

Abstract : Similarity solutions are presented for the compressible laminar boundary layer with adverse pressure gradients showing the quantitative effect of heat and mass transfer on the wall shear and temperature gradient. Two suction parameters as well as wall temperatures ranging from absolute zero to twice the free-stream stagnation temperature are investigated for numerous adverse pressure gradients.

Descriptors :   (*LAMINAR BOUNDARY LAYER, *TWO DIMENSIONAL FLOW), MASS TRANSFER, HEAT TRANSFER, COMPUTER PROGRAMS, STAGNATION POINT, SHEAR STRESSES, VELOCITY, ENTHALPY, WALLS, COMPRESSIBLE FLOW, KINEMATICS, VISCOSITY, SEPARATION

Subject Categories : Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE