thrust_drag - [ Cl = 2.0 * W / (rho * S * V ^ 2); C Cd =...

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function [F] = thrust_drag(h, V) f rhostar = 7.0163e-4; %slugs/ft^3 W = 11000; %lbs S = 232; %ft^2 S [temp,pres,rho,sos] = atmos62(h); [ M = V / sos; M [Cd0, K] = parabolicdrag(M);
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Unformatted text preview: [ Cl = 2.0 * W / (rho * S * V ^ 2); C Cd = Cd0 + K * Cl ^ 2; C F = (2000 * (rho / rhostar) * (0.89 * (M - 0.4) ^ 2 + 0.64)) - (0.5 * rho * Cd * S * V ^ 2);...
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This note was uploaded on 09/18/2011 for the course ASE 167M taught by Professor Staff during the Spring '10 term at University of Texas at Austin.

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