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