Ajet airplane, with a wing area of 20 m', moves through still air at a constant velocity of 225 m/s. the plane is at an altitude of 5000 m and is climbing at an angle of 20 degrees horizon. under the given conditions, the plane has a lift coefficient of 0.2, and with the a drag coefficient of 0.075. answer the following a)-what thrust force, in n, must the jet engine produce? b)-what power, in kw, must the jet engine produce?

the equation above shows how temperature f, measured in degrees fahrenheit, relates to a temperature c, measured in degrees celsius. based on the equation, which of the following must be true?

a temperature increase of 1 degree fahrenheit is equivalent to a temperature increase of

5

9

degree celsius.

a temperature increase of 1 degree celsius is equivalent to a temperature increase of 1.8 degrees fahrenheit.

a temperature increase of

5

9

degree fahrenheit is equivalent to a temperature increase of 1 degree celsius.

a) i only

b) ii only

c) iii only

d) i and ii only

answer:

i dont know the answer but good luck

explanation: