Welcome to EssayHotline!

We take care of your tight deadline essay for you! Place your order today and enjoy convenience.

Calculate the tail rotor thrust required to trim the helicopter in hover.

Continued overleaf Page 2 of 3 Q1 A helicopter has a main rotor speed of 260 rpm, and a main rotor radius R=5.90m. The gross take-off weight is 30kN. The blades have an average drag coefficient of CD=0.01, and the rotor solidity =0.08. The distance between the axis of the main and tail rotor is […]

© 2024 EssayHotline.com. All Rights Reserved. | Disclaimer: for assistance purposes only. These custom papers should be used with proper reference.