Accession Number : ADA308103
Title : Joint Research on Computational Fluid Dynamics and Fluid Flow Control.
Descriptive Note : Final rept. 1 Jun 92-30 Nov 95,
Corporate Author : CALIFORNIA UNIV LOS ANGELES DEPT OF MECHANICAL AEROSPACE AND NUCLEAR ENGINEER ING
Personal Author(s) : Gibson, J. S.
PDF Url : ADA308103
Report Date : 30 NOV 1995
Pagination or Media Count : 64
Abstract : This research project has developed methods for computational fluid dynamics and fluid-flow control. The research on computational fluid dynamics has consisted of the analysis and development of simulations and mathematical models of two-dimensional fluid motion. The control research has used a hierarchy of simulations and models t design feedback controllers for fluid flows. Both adaptive and nonadaptive controllers were developed. The research was motivated by the need to stabilize high Reynolds number flows around bodies such as delta wing aircraft.
Descriptors : *COMPUTATIONAL FLUID DYNAMICS, *BOUNDARY LAYER FLOW, MATHEMATICAL MODELS, ADAPTIVE CONTROL SYSTEMS, HIGH RATE, AIRCRAFT, VORTICES, FINITE DIFFERENCE THEORY, FEEDBACK, NONLINEAR ANALYSIS, TWO DIMENSIONAL FLOW, FLUID CONTROL, DELTA WINGS, REYNOLDS NUMBER.
Subject Categories : Fluid Mechanics
Distribution Statement : APPROVED FOR PUBLIC RELEASE