%% Calculate normal shock1
%% Calculate normal shock1
% Calculate the normal shock relations for air (gamma = 1.4) for total pressure ratio of 0.61.

[mach, T, P, rho, downstream_mach, P0, P1] = flownormalshock(1.4, 0.61, 'totalp')

% Copyright 2015 The MathWorks, Inc.