Accession Number : AD0266501

Title :   THE METHOD OF INTEGRAL RELATIONS FOR CONICAL FLOW - THEORETICAL ANALYSIS

Corporate Author : GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE N Y

Personal Author(s) : BROOK,JOHN W.

Report Date : OCT 1961

Pagination or Media Count : 1

Abstract : The gas dynamic equations in orthogonal conical coordinates are integrated across one strip, following the idea of Dorodnitsyn's method of integral relations. Although no numerical results are obtained, a discussion of the resulting ordinary differential equations or the case of an elliptic cone and a flat-plate delta wing is presented. (Author)

Descriptors :   *AERODYNAMIC CHARACTERISTICS, *GAS FLOW, *SHOCK WAVES, CONICAL BODIES, DELTA WINGS, DIFFERENTIAL EQUATIONS, FLUID MECHANICS, INTEGRAL EQUATIONS, MATHEMATICAL ANALYSIS, PARTIAL DIFFERENTIAL EQUATIONS

Distribution Statement : APPROVED FOR PUBLIC RELEASE