Reduce Thrust ➤ Nose will Drop
Increase Thrust ➤ Nose will Raise
A force acting on a point can be broken up into it’s horizontal (x) and vertical (y) components:
This is relevant to aviation when we manoeuvre the aircraft…
Thrust needs to be greater to overcome the 2 rearward forces from drag & the rearward component of weight:
Increasing Power improves Climb Performance
Definitions:
Another option is a Cruise Climb which prioritises least time to destination.
Maximum Angle of Climb (AoC) occurs at the airspeed and Angle of Attack combination which allows the maximum excess thrust.
Maximum Rate of Climb (RoC) for a typical propeller airplane occurs at an airspeed and Angle of Attack combination closer to L/DMAX.
Increasing weight reduces climb performance!
Climb of a piston aircraft usually occurs at full power, thus any reduction in power will reduce climb performance.
Any change in airspeed away from Best Rate / Angle of Climb point will result in reduced climb performance. That is, we need more power or more speed to achieve our best the same performance!
Climb performance reduces as altitude increases due to the thinner air at higher altitudes
The effect of Flap depends on how much of the flaps are extended into the airflow.
Lift and Drag are constant for the same speed! The remaining forces effect glide:
We enter a powered descent!
The descent angle is reduced and the forward component of weight is less:
Lowering flaps increases drag!
To maintain speed the nose is lowered and a steeper Angle of Descent (AoD) is achieved.