Accession Number : AD0749843

Title :   Induced Velocities of Free Wing Vortices with a Curved Axis in a Plane,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Kondrat,K. I.

Report Date : 04 AUG 1972

Pagination or Media Count : 11

Abstract : The report calculates induced velocities of a wing with a curved axis not perpendicular to the velocity of the incoming flow. The velocity produced at each point of the surrounding space by the wing vortex system will consist of two parts: the velocity created by the vortex sheet and the velocity created by the lifting vortex line. The calculation of the velocity created by the wing vortices is the content of this article. (Author)

Descriptors :   (*WINGS, VORTICES), LIFT, AIRFOILS, FLUID FLOW, NUMERICAL ANALYSIS, USSR

Subject Categories : Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE