- #1
Ryansf98
- 15
- 0
Homework Statement
"Figure 5 depicts a 30 000 kg aircraft climbing at an angle θ = 15˚ when the thrust T = 180 kN. The aircraft’s speed is 300 km/hr and its acceleration is 2m/s2. If the radius of curvature of the path is 20 km (i.e., θ is decreasing), compute the lift and drag forces on the aircraft."
a = 2m/s^2
T = 150000N
Theta = 15 degrees
Radius of Curvature (K) = 20000m
v = 300km/hr => v = 83.3 m/s^1
Homework Equations
W=mg, F=ma, a = v^2/K
The Attempt at a Solution
I was going to treat this similar to an object moving up an inclined plane. Although, I don't know if this would work.
I determined W = mg, W= 294,300N.
I then thought using a = 83.3^2/20000 = 0.35 m/2^1.
Therefore, F = ma, F = 30,000 * 0.35 = 10,500N.
Therefore F + F(f) (i.e. Wsin(Theta)) = Drag.
Upon calculating, I got close to the answer for drag but I believe only by coincidence. As I considered you would have to work out normal and tangential components individually, therefore a= v^2/K would be in the normal direction, not the tangential like I used it for.
I also am unsure on how to calculate Lift if I cannot treat this an incline plane problem.