Accession Number : AD0615901

Title :   NEW APPROACH TO THE TWO-DIMENSIONAL HYPERSONIC BLUNT BODY PROBLEM.

Descriptive Note : Interim technical rept.,

Corporate Author : CINCINNATI UNIV OHIO

Personal Author(s) : Hida,Kinzo

Report Date : JAN 1965

Pagination or Media Count : 27

Abstract : Hypersonic flow past a two-dimensional blunt body was treated by making use of the technique of the perturbation of independent variables. Application to a flat plate normal to the oncoming flow leads us to the same results as those obtained by Cole and Brainerd due to a different procedure. One more term is found for the stand-off distance of a shock wave. The case past an arbitrary body is also considered. (Author)

Descriptors :   (*HYPERSONIC FLOW, BLUNT BODIES), (*BLUNT BODIES, HYPERSONIC FLOW), TWO DIMENSIONAL FLOW, DELTA WINGS, DIFFERENTIAL EQUATIONS, SHOCK WAVES, INCOMPRESSIBLE FLOW, SERIES(MATHEMATICS), NUMERICAL ANALYSIS

Distribution Statement : APPROVED FOR PUBLIC RELEASE