Accession Number : AD0686818

Title :   THE EXTENT OF LAMINAR, TWO-DIMENSIONAL BOUNDARY LAYER SEPARATION DUE TO A COMPRESSION CORNER AT MODERATELY HYPERSONIC SPEEDS,

Corporate Author : SYSTEMS RESEARCH LABS INC DAYTON OHIO

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

Report Date : JAN 1969

Pagination or Media Count : 25

Abstract : A simple technique is presented for estimating the extent of separation of a two-dimensional laminar boundary layer including effects of Mach number, Reynolds number, and heat transfer. Quantitative effects of these parameters are discussed for moderately hypersonic speeds. (Author)

Descriptors :   (*FLOW SEPARATION, HYPERSONIC CHARACTERISTICS), LAMINAR FLOW, TWO DIMENSIONAL FLOW, BOUNDARY LAYER, COMPRESSIBLE FLOW, MACH NUMBER, REYNOLDS NUMBER, HEAT TRANSFER

Subject Categories : Aerodynamics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE