Accession Number : AD0695985
Title : LOW-ASPECT-RATIO WING FLYING ABOVE AN INTERFACE BETWEEN FLUIDS OF DIFFERENT DENSITY.
Descriptive Note : R. E. Gibson Library bulletin translation series,
Corporate Author : JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Personal Author(s) : Putilin,S. I.
Report Date : 05 SEP 1969
Pagination or Media Count : 13
Abstract : An approximate theory is developed for a low-aspect-ratio wing moving above the interface of two fluids of different density. The main feature of the theory consists in the replacement of the exact value of the velocity potential by its value obtained at a great distance downstream from the wing. (Author)
Descriptors : (*HYDROFOILS, AERODYNAMIC CHARACTERISTICS), GROUND EFFECT MACHINES, AIR, WATER, INTERFACES, GROUND EFFECT, ASYMPTOTIC SERIES, HARMONIC ANALYSIS, USSR
Subject Categories : Surface Effect Vehicles & Amphibious Vehicles
Distribution Statement : APPROVED FOR PUBLIC RELEASE