Aerodynamic Unaccelerated Performance
In this module week, you will apply your gained knowledge about unaccelerated aircraft performance of the Cessna 172 Lyc. IO-360-L2A . Since you will build on your previously derived drag data for your example aircraft. For your independent project, create an instructional presentation. Using/building on your previous drag (i.e., thrust-required) table and graph created in … Read more