Engineering, 14.12.2021 05:00 annafellows

Your aircraft (Weight = 2000 N) is about to take off with a lift coefficient of CL = 0.9. Perform the following calculations and show all your work: 1- Take off Speed (Hint: Assume that your wing Area is 10 m^2 and that the take off is happening at sea level where density is rho = 1.225 Kg/m^3 - Ignore the effect of the stabilizer on lift).

2- Lift coefficient at altitude assuming a cruising speed V= 225 m/s (Hint: Apply the same formula as before)

Which condition will be closer to the stall velocity? Explain why.

Answers: 1

Show answers

Other questions on the subject: Engineering

Engineering, 04.07.2019 18:10, siri5645

At 12 noon, the count in a bacteria culture was 400; at 4: 00 pm the count was 1200 let p(t) denote the bacteria cou population growth law. find: (a) an expression for the bacteria count at any time t (b) the bacteria count at 10 am. (c) the time required for the bacteria count to reach 1800.

Answers: 1

continue

Engineering, 04.07.2019 18:10, Fahaddie

The thermal expansion or contraction of a given metal is a function of the f a)-density b)-initial temperature c)- temperature difference d)- linear coefficient of thermal expansion e)- final temperature f)- original length

Answers: 2

continue

Engineering, 04.07.2019 18:10, Talos02

Burgers vector is generally parallel to the dislocation line. a)-true b)-false

Answers: 2

continue

Engineering, 04.07.2019 19:10, Destinationz

Asteam is contained in a rigid tank with a volume of 1 m3. initially, the pressure and temperature are 7 bar and 500 oc, respectively. the temperature drops due to cooling process. determine: (1) the temperature at which condensation begins in °c, (2) the fraction of the total mass that has condensed when the pressure decreased to 0.5 bar. (3) the volume in m3 occupied by saturated liquid at the final state?

Answers: 3

continue

You know the right answer?

Your aircraft (Weight = 2000 N) is about to take off with a lift coefficient of CL = 0.9. Perform th...