Please I need help on this asap thank you Find the Total Energy (ft-lb) of an ai

Question

Please I need help on this asap thank you

Find the Total Energy (ft-lb) of an aircraft weighing 20,000 lbs at 5,000 ft true altitude and 200 KTS True Air Speed. Find Vertical Velocity in ft/min for an aircraft in a 200 KTAS climb with a climb angle of 10 deg (assume no wind). What would be the length of the takeoff run (ft)? GIVEN INFORMATION: Use "g" = 32.2ft/s2 1 knot = 1.69 ft/s Gross Weight = 20,000 pounds Average Drag = 2,000 pounds Average Friction Force = 400 pounds Average Thrust = 10,000 pounds Lift Off Speed = 125 KTAS On a takeoff roll, which of the Newton's laws of motion apply? (An airplane is starting on the runway at zero ground speed and thrust is added and the airplane accelerates and then takes off after gaining enough speed to create lift).

Explanation / Answer

1)B

2)B

3)A

4)C

5)D

6)D

7)E

8)A

9)B

Related Questions

Navigate

• Browse (All)
• Browse P
• Subjects

---