Accession Number : AD0775108

Title :   On the Solution to the Problem of the Flow around a V-Shaped Wing with an Intense Shock Wave on the Leading Edge,

Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO

Personal Author(s) : Lapygin,V. I.

Report Date : 01 FEB 1974

Pagination or Media Count : 14

Abstract : A report is made on the effect of initial and boundary conditions on the numerical solution to the problem of the flow around a V-shaped wing with supersonic leading edges.

Descriptors :   *Swept wings, *Supersonic characteristics, *Flow fields, Numerical analysis, Leading edges, Wedges, Shock waves, Angle of attack, Translations, USSR

Subject Categories : Aerodynamics

Distribution Statement : APPROVED FOR PUBLIC RELEASE