solve for this Implement a computer program to solve the combined Blade Element Momentum Theory (BEMT) equations numerically. The program should be able to accept arbitrary rotor geometry and output both sectional performance quantities as well as integrated rotor quantities. - For an ideally twisted rotor with rectangular planform ( =0.1 ) compare the predicted inflow as a function of blade span with the exac (analytic) result when the rotor is operating in hover at a CT=0.008. Plot the analytical solution as a solid line and use discrete symbols for ealculations. - For the same conditions, also show the radial distributions of thrust, induced torque, and lift coefficient. Compare these distributions with the analyical solution. In each ease, plot the analytical solution as a solid line and use discrete symbols for your numerical results. - Compare the numerical calculations of integrated thrust and induced power with analytical results for this rotor wer the range 0CT0,01..

1. solve for this
Implement a computer program to solve the combined Blade Element Momentum Theory
(BEMT) equations numerically. The program should be able to accept arbitrary rotor geometry
and output both sectional performance quantities as well as integrated rotor quantities. - For an
ideally twisted rotor with rectangular planform ( =0.1 ) compare the predicted inflow as a
function of blade span with the exac (analytic) result when the rotor is operating in hover at a
CT=0.008. Plot the analytical solution as a solid line and use discrete symbols for ealculations. -
For the same conditions, also show the radial distributions of thrust, induced torque, and lift
coefficient. Compare these distributions with the analyical solution. In each ease, plot the
analytical solution as a solid line and use discrete symbols for your numerical results. - Compare
the numerical calculations of integrated thrust and induced power with analytical results for this
rotor wer the range 0CT0,01.