Flow parameters in chart form and calculated for air as real gas in chemical equilibrium for series of stagnation temperatures between 2790 and 4950 R and pressures up to 1000 atm; from these charts it is possible to calibrate hypersonic nozzle in conventional way; method for calculating inviscid nozzle contour including real-gas effects.


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    Title :

    Study of equilibrium real-gas effects in hypersonic air nozzles, including charts of thermodynamic properties for equilibrium air


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    179 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :