Question: The minimum sink rate is attained by flying at a relative airspeed of u/\sqrt[4]{3}.
Options
A : TRUE
B : FALSE
C : -
D : -
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Climb and Descent Performance with Thrust-Producing Engines more questions
The airspeed chosen for after take-off climb should be same....
The best gradient of climb is attained at the time....
The best gradient of climb is predicted to be at....
The best rate of climb occurs when the excess thrust....
The departure path in an airport is depended on ___
What is the benefit of flying at minimum power speed?
What is the correct formula for dimensionless rate of climb?
What is the distance of the safeguard path?
What is the gradient of climb for one engine inoperative?
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