Accession Number : AD0883521
Title : Comparison of Experimental Pressure Distributions with Those Calculated by the Douglas Neumann Program,
Corporate Author : DOUGLAS AIRCRAFT CO LONG BEACH CA
Personal Author(s) : Faulkner, Sue ; Hess, John L. ; Giesing, Joseph P.
Report Date : 01 DEC 1964
Pagination or Media Count : 99
Abstract : This report presents a series of graphical comparisons of experimental pressure distributions with pressure distributions calculated by the Douglas Neumann Program. The configurations considered have been classified geometrically as: axisymmetric bodies at zero or nonzero angle of attack, two-dimensional lifting airfoils, and truly three-dimensional bodies. Within each category a variety of bodies are presented including multiple bodies, and both low-speed and high subsonic flows are shown. This report contains essentially every case for which the results of the calculations have been compared with experiment. The agreement is very satisfactory in all cases except for a few very complicated configurations that could not be defined well enough for good accuracy; and even in such cases the calculation gives results that are usable for many purposes. (Author)
Descriptors : *COMPUTER PROGRAMS), (*FLOW FIELDS, PRESSURE), (*FLUID FLOW, NUMERICAL METHODS AND PROCEDURES, COMPRESSIBLE FLOW, SUBSONIC FLOW, SONAR DOMES, JET AIRCRAFT, DESTROYERS, EXTERNAL STORES, HYDROFOILS, LIFT, WINGS, ANGLE OF ATTACK, SHROUDED PROPELLERS, DIGITAL COMPUTERS, SHIP HULLS, VISCOSITY, JET ENGINE NACELLES, VELOCITY, ACCURACY, ERRORS, AERODYNAMICS, HYDRODYNAMICS.
Subject Categories : Aircraft
Computer Programming and Software
Distribution Statement : APPROVED FOR PUBLIC RELEASE