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.
Study of equilibrium real-gas effects in hypersonic air nozzles, including charts of thermodynamic properties for equilibrium air
NASA -- Tech Note
1960
179 pages
Report
English
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