In straight and level flight all the forces are said to in?
Equilibrium
What is the load factor in straight and level flight
1
In a straight and steady climb the load factor will be?
Less than 1
LF =
Weight
Flight path angle =
Horizontal axis and flight path
Pitch angle =
Flight path angle + AOA
What is the equation for lift with weight in a straight and steady climb
L = W x Cos (gamma - flight path angle)
Gradient percentage =
T-D
——- x 100
Weight
For every 3 degrees what is the % of gradient
5
What speed gives the greatest gradient of climb
Vx
Vx is calculated where there is?
Greatest excess thrust (Vmd for a jet, near the stall speed for a prop)