Performance

The most important data on the aircraft is known, therefore we can recalculate the performance it will actually have. In subsection 3.2, we plotted the instantaneous turnrate with aspect to W/S, solving equations in subsection 3.3 gives the maximum level speed. The maximum rate of climb at a given speed is found evaluating:

is simply the excess power at a given situation, expressed in such a way that it directly transforms to rate of climb in if the speed remains constant.

The resulting performance of the aircraft is, in addition to the fact that it can do the design mission stated in section 1:

• Take off ground roll
• Landing ground roll
• Instantaneous turn rate:
• Max level speed: @
• Rate of climb: , , sea level.