
Accession Number : AD0809388
Title : THEORETICAL INVESTIGATIONS OF BOUNDARY LAYER STABILITY.
Descriptive Note : Final rept. Jul 63Aug 64,
Corporate Author : NORTHROP CORP HAWTHORNE CA NORAIR DIV
Personal Author(s) : Brown, W. Byron ; Raltz, Gibbs S.
Report Date : SEP 1966
Pagination or Media Count : 126
Abstract : The mathematical analysis underlying a Fortran program for calculating the proper solutions of the OrrSommerfeld system with sufficient accuracy and economy for applying the resonance theory of transition is described. This program covers spacewise growths, rather than timewise growths as in previous computations, of mainly twodimensional Fourier components of the motion. It employs various innovations providing as much accuracy from efficient singleprecision arithmetic as would be obtained from awkward multipleprecision arithmetic in previous calculation schemes. The source programs and some sample calculations, for the proncipal mode of oscillation of the Blasius boundary layer, are included. The LeesLin stability equation for compressible flow have been extended to include the terms involving the component of the mean boundary layer flow perpendicular to the flat plate. At Mach 5 this more than doubled the critical Reynolds number. Allowance was then made for the threedimensional aspect of the disturbance velocity. The final result was to give good agreement with observed data in the lower branch of the neutral stability curve at Mach 2.2 and Mach 5, fair agreement with the upper branch at Mach 2.2 and large discrepancies with the data in the upper branch at Mach 5. Comparison of experimental determined neutral stability curves with those computed by simplified approximations have disagreed considerably at high Mach numbers on the upper branch, even when agreement was fairly good on the lower branch.
Descriptors : (*BOUNDARY LAYER, STABILITY), THEORY, LAMINAR BOUNDARY LAYER, BOUNDARY LAYER TRANSITION, COMPUTER PROGRAMS, MATHEMATICAL ANALYSIS, COMPRESSIBLE FLOW, TWO DIMENSIONAL FLOW, INCOMPRESSIBLE FLOW, RESONANCE, MOTION, FLAT PLATE MODELS, EXPERIMENTAL DATA, HYPERSONIC FLOW, SUPERSONIC FLOW, REYNOLDS NUMBER.
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE