Accession Number : AD0467786

Title :   INVISCID HIGH TEMPERATURE HYPERSONIC FLOW OF AIR PAST POINTED BODIES OF REVOLUTION.

Descriptive Note : Quarterly interim technial rept., 30 Jun-30 Sep 64,

Corporate Author : ALABAMA UNIV HUNTSVILLE RESEARCH INST

Personal Author(s) : Thoenes,Jurgen ; Hermann,Rudolf

Report Date : OCT 1964

Pagination or Media Count : 35

Abstract : The gas model and the thermodynamic equations were thoroughly checked and rederived. The equations of motion governing the flow past any object were derived with respect to an orthogonal curvilinear coordinate system, suitable for a large group of bodies of rather general shape. Boundary conditions (shock relations) were obtained for chemically frozen and for equilibrium flow. As for the solution of the system of governing equations, Dorodnitsyn's method of integral relations (direct method) was studied in general. Specializing the general method, all the necessary equations for the first approximation were derived. (Author)

Descriptors :   (*HYPERSONIC FLOW, BODIES OF REVOLUTION), (*HIGH TEMPERATURE, AIR), (*CONICAL BODIES, HYPERSONIC FLOW), AERODYNAMIC HEATING, EQUATIONS OF STATE, ENTHALPY, POLYNOMIALS, PARTIAL DIFFERENTIAL EQUATIONS, MATHEMATICAL MODELS

Distribution Statement : APPROVED FOR PUBLIC RELEASE