0/5 pts
Question 2
2nd Problem Statement. At the instant shown, the airplane has a velocity, v= 270 mls in the x direction. The plane has mass 11,00
thrust, T = 110kN, lit, L = 260kN and drag, D = 34. Which of the following equations best represents the sum of forces in the Grection?
T
150
Path
150
Horizontal
mg
Stv