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
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE