Chapter 19: Climb Flashcards
Climb Angles (3)
Flight Path - groud to RAF
3D AoA - RAF to AC longitudinal
Pitch Angle - ground to AC longitudinal
Fligh Path Angle Calculation
sin(γ) = ( T - D ) / W
Climb Load Factor
n < 1
Best Angle Climb (Jet)
Velocity, Explanation
Thrurst is constant with speed
Vx @ Vmd
Best Angle Climb (Piston)
Velocity, Explanation
Thrust decreases with velocity
Vx near Vs (dangerous)
Instead use Vmp
Climb Gradient
Gradient Calculation, Justification?
Gradient Relationship to Flight Path Angle
G = height / distance = tan (y)
at small angles, tan(y) = sin(y)
so G = ( T - D ) / W
3° = 5%
Flight Path Angle vs Pitch
can it be negative?
Flight path angle > 0
pitch can be negative or positive
Flight Path Angle vs Climb Angle
Difference
Flight Path Angle = with headwind / tailwind
Climb angle = theoretical value based on T, D, W