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v1.0 must do the following as a Matlab script: - Accept a nozzle profile and predict M, P, and T over the profile for quasi-1D flow - Determine whether the flow contains normal shocks and the location of such shocks - Plot these parameters versus the x-axis, including the shock cases. - Output critical and exit parameters for M, P, T, mdot - Predict and output thrust and specific impulse - Match known validation cases v1.0 may not, but future versions should: - Work on multiple platforms - Have a GUI - Handle cases other than non-reacting, homogeneous gas propellants without heat addition - Predict performance 2D by the method of characteristics - Take performance losses due to geometry or assumptions into account
Overdue by 9 year(s)•Due by May 20, 2017•1/9 issues closed