Accession Number : ADA195559
Title : A Study of the Effect of Random Input Motion on Low Reynolds Number Flows.
Descriptive Note : Final rept. Sep 85-Nov 87,
Corporate Author : SOUTHWEST RESEARCH INST SAN ANTONIO TX
Personal Author(s) : Unruh, James F. ; Park, Joel T. ; Johnson, James E.
Report Date : MAY 1988
Pagination or Media Count : 64
Abstract : The SwRI large water tunnel was modified by the addition of a large test section (.71 m x .81 m x 1.8 m long) to provide low Reynolds number flows with low blockage for models in a highly separated flow condition. Flow characteristics are documented and other physical features are described. The feasibility of conducting water tunnel experiments involving unsteady aero-hydrodynamics was demonstrated by performing a series of flow visualization studies on a oscillating airfoil (NACA 0012). This experiment was carried out at a reduced fully separated until 17 degress angle of attack, and the downstream wash of the separated flow occurred at 22 degrees. (mjm)
Descriptors : *FLOW, *REYNOLDS NUMBER, *WATER TUNNELS, AIRFOILS, ANGLE OF ATTACK, FLOW SEPARATION, FLOW VISUALIZATION, INPUT, LOW RATE, MOTION, OSCILLATION, TEST EQUIPMENT.
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE