Accession Number : AD0744143

Title :   Hypersonic Flow around a Thin Three-Dimensional Body,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Dzvonyk,L. I.

Report Date : 28 MAR 1972

Pagination or Media Count : 9

Abstract : Hypersonic nonviscous flow about a thin three-dimensional body of triangular wing shape was investigated. In the framework of asymptotic theory of small perturbations, equations of motion and boundary conditions for the general class of perturbations were obtained. Flow about such a body is divided into two regions: an external region of uniform flow and a central region with conical flow. The first region is examined in the present paper. (Author)

Descriptors :   (*DELTA WINGS, HYPERSONIC CHARACTERISTICS), MATHEMATICAL MODELS, FLOW FIELDS, EQUATIONS OF MOTION, THREE DIMENSIONAL FLOW, USSR

Subject Categories : Aerodynamics
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE