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 OH

Personal Author(s) : Ball, Karlheinz O

PDF Url : AD0686818

Report Date : Jan 1969

Pagination or Media Count : 26

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.

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

Subject Categories : Aerodynamics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE