Accession Number : AD0695984
Title : MOTION OF A THIN AIRFOIL AT ARBITRARY DISTANCES FROM A SOLID AND A FLUID BOUNDARY.
Descriptive Note : R. E. Gibson Library bulletin translation series,
Corporate Author : JOHNS HOPKINS UNIV SILVER SPRING MD APPLIED PHYSICS LAB
Personal Author(s) : Berkovskii,B. S. ; Koshevoi,V. I.
Report Date : 27 AUG 1969
Pagination or Media Count : 16
Abstract : The aerodynamics of lifting systems flying at arbitrary distances from a boundary are discussed. The problem is solved by the kernel degeneration method through reduction of a singular equation of the first kind into a Fredholm equation of the second kind. The coefficients of the system of algebraic equations appearing in the solution of the Fredholm equation can be determined to any degree of accuracy by means of a computer. (Author)
Descriptors : (*THIN WINGS, AERODYNAMIC CHARACTERISTICS), LIFT, INTEGRAL EQUATIONS, FORCE(MECHANICS), MOMENTS, INTERFACES, USSR
Subject Categories : Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE