Hi All
I am doing a project for my final year of aerospace design. To do that I have to work out the Drag Polar of the Cessna Citation X. From that I have to work out the Performance of the aircraft, then design my own one and calculate the new design that I will be doing, then compare it to show that my design will be improved in terms of Aerodynamic and noise reduction.
Your help will be highly appreciated. Please feel free to ask any question
Many Thanks
I am doing a project for my final year of aerospace design. To do that I have to work out the Drag Polar of the Cessna Citation X. From that I have to work out the Performance of the aircraft, then design my own one and calculate the new design that I will be doing, then compare it to show that my design will be improved in terms of Aerodynamic and noise reduction.
Your help will be highly appreciated. Please feel free to ask any question
Many Thanks