NASA Technical Reports Server (NTRS) 19750006919: Effects of vibrational nonequilibrium on the inviscid design of an axisymmetric nozzle for hypersonic flowReport as inadecuate




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An axisymmetric, hypersonic nozzle for arc-heated air is described. The method of characteristics is used to compute an inviscid nozzle contour in which vibrational nonequilibrium is approximated by the sudden-freeze technique. Chemical reactions are shown to freeze early in the nozzle expansion, and the result of vibrational and chemical freezing

Author: NASA Technical Reports Server (NTRS)

Source: https://archive.org/







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