Accession Number : AD0700418
Title : LINEAR PROBLEMS IN THE HYDRODYNAMIC STUDY OF A WING FLYING ABOVE THE INTERFACE BETWEEN FLUIDS OF DIFFERENT DENSITIES.
Descriptive Note : R. E. Gibson Library bulletin translation series,
Corporate Author : JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Personal Author(s) : Panchenkov,A. N.
Report Date : 15 SEP 1969
Pagination or Media Count : 24
Abstract : The acceleration potential method is applied to the solution of linear problems arising in incompressible flow past a wing positioned above the interface between fluids of different densities. Some general results obtained for problems involving the motion of lifting wings at high Froude numbers are discussed. Simple formulas are derived for a wing in two-dimensional flow and for a high-aspect-ratio, finite-span wing. An exact formulation of the problem is obtained for small density ratios. (Author)
Descriptors : (*GROUND EFFECT MACHINES, *INCOMPRESSIBLE FLOW), (*WINGS, AERODYNAMIC CHARACTERISTICS), SUBSONIC FLOW, LINEAR SYSTEMS, INTERFACES, LIFT, TWO DIMENSIONAL FLOW, ASPECT RATIO, DENSITY, USSR
Subject Categories : Aerodynamics
Surface Effect Vehicles & Amphibious Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE