Straight And Level And Climbing Flight Flashcards
Thrust must equal
Drag + Wsin0
Lift Must Equal
Lift = Wcos0
Steady Climb
L = WCOS0
T = D + WSIN0
Weight is greater than lift
Thrust is greater than drag
Descending Flight
D = Thrust + Wsin0
L = Wcos0
Weight is greater than lift
Drag is greater than thrust
Maximum Range in glide is obtained by flying at
VMD
Mass effect on gliding
Glide range independent of mass
Rate of descent - heavy aircraft higher airspeed therefore faster towards ground
Headwind component on climb
Increase the flight path angle
Slower ground speed
Same airspeed
Shorter ground distance
Tail wind component on climb
Decrease the flight path angle
Greater ground speed
Same air speed
Longer ground distance
Flight path angle
Gradient related to ground distance (takes wind into account)
Angle of climb
Relative to still air does not take wind into account