Accession Number : AD0413074
Title : HYPERSONIC FLOW PAST AXISYMMETRIC BODIES FLYING AT AN ANGLE OF ATTACK,
Corporate Author : FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Personal Author(s) : Minostsev,B.B.
Report Date : 14 JUN 1963
Pagination or Media Count : 20
Abstract : The solution of the problem of the flow of an ideal gas moving at high supersonic velocity past axisymmetric bodies at angle of attack is pre sented. The problem was solved by expanding the unknown characteristics of the flow into a series with respect to parameter epsilon (gamma 1)/(gamma 1). The problem was solved in the first approximation in quadratures. (Author)
Descriptors : (*HYPERSONIC FLOW, BOUNDARY), (*ANGLE OF ATTACK, AXIALLY SYMMETRIC), DENSITY, MOTION, VELOCITY, SUPERSONIC, SHOCK WAVES, GASES, PARTIAL, DIFFERENTIAL EQUATIONS, OPERATORS (MATHEMATICS), PRESSURE, BLUNT BODIES.
Distribution Statement : APPROVED FOR PUBLIC RELEASE