Accession Number : ADA181301
Title : Boundary Layer Separation in 2 and 3 Dimensional High Speed Blow.
Descriptive Note : Final rept. May 83-Apr 84,
Corporate Author : CALIFORNIA UNIV BERKELEY COLL OF ENGINEERING
Personal Author(s) : Holt,Maurice
PDF Url : ADA181301
Report Date : May 1987
Pagination or Media Count : 11
Abstract : Laminar boundary flow on cones in supersonic flow was calculated using a modified Method of Integrals to account for the change in velocity profiles in the separated regions. The work was extended to three dimensions and compared to experimental data. Significant progress was made in the modeling of th flows and in particular the regions of separated and reverse flow in the boundary layer.
Descriptors : *SECONDARY FLOW, *SUPERSONIC FLOW, *FLOW SEPARATION, *BOUNDARY LAYER FLOW, BOUNDARY LAYER, INTEGRALS, LAMINAR BOUNDARY LAYER, LAMINAR FLOW, PROFILES, SEPARATION, VELOCITY, THREE DIMENSIONAL FLOW, TWO DIMENSIONAL FLOW, HIGH ANGLES, ANGLE OF ATTACK, CONICAL BODIES
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE