Accession Number : AD0705581
Title : SIMILAR SOLUTIONS OF THE ATTACHED AND SEPARATED COMPRESSIBLE LAMINAR BOUNDARY LAYER WITH HEAT TRANSFER AND PRESSURE GRADIENT.
Descriptive Note : Final rept.,
Corporate Author : AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Christian,James W. ; Hankey,Wilbur L. ; Petty,James S.
Report Date : FEB 1970
Pagination or Media Count : 116
Abstract : The development of governing equations and tabulation of similar solutions to the two-dimensional, laminar, compressible boundary layer with heat transfer are presented. Similar velocity and temperature profiles and global quantities such as displacement thickness, momentum thickness, form factor, etc., are presented for 116 pressure gradient-heat transfer combinations. Surface temperatures for these cases range from absolute zero (S(0) = - 1) to twice the free stream stagnation temperature (S(0) = + 1), while the streamwise pressure gradient varies from values corresponding to maximum reversed flow (beta=-0.36) to those of extremely accelerated flows (beta = 20). Results are presented at regular intervals of the parameters S(0) and beta, allowing for straight-forward comparisons between cases. Five decimal place accuracy is maintained for all results. (Author)
Descriptors : (*LAMINAR BOUNDARY LAYER, *HEAT TRANSFER), (*COMPRESSIBLE FLOW, TWO DIMENSIONAL FLOW), FLOW SEPARATION, TABLES(DATA), PRESSURE, DIFFERENTIAL EQUATIONS
Subject Categories : Aerodynamics
Distribution Statement : APPROVED FOR PUBLIC RELEASE