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Optimizing Mach-R System for Efficient Flight Performance

Explore the Mach-R system with varying parameters to enhance aircraft performance and stability. Analyze impact of g, energy, gravity, and more to achieve optimal results.

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Optimizing Mach-R System for Efficient Flight Performance

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  1. %% PPLANE file %% H.name = 'mach_r_system.pps'; H.xvar = 'x'; H.yvar = 'y'; H.xder = '1'; H.yder = '(1+(g-1)*y/2)*(2*E/x-((5-3*g)/(g-1))*GM/2/r0/x^2)/(E+GM/r0/x)*(2*y/(y-1))'; H.pname = {'g','E','GM','','r0',''}; H.pval = {'1.4','-.4','4','','1',''}; H.fieldtype = 'none'; H.npts = 20; H.wind = [0 1 0 1];

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