A 13500 kg airplane has a wing loading of 2.75 kN/m2. At 8° angle of attack the lift coefficient is 0.61. What is the sp
Posted: Tue Jun 07, 2022 6:02 pm
A 13500 kg airplane has a wing loading of 2.75 kN/m2.
At 8° angle of attack the lift coefficient is 0.61. What is the
speed (in knots) necessary to maintain horizontal flight at this
angle of attack at sea-level? Round off your answer to the ones
place. Indicate only the numeric value of your response.
At 8° angle of attack the lift coefficient is 0.61. What is the
speed (in knots) necessary to maintain horizontal flight at this
angle of attack at sea-level? Round off your answer to the ones
place. Indicate only the numeric value of your response.