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An aeroplane needs 2.5 degrees more up elevator for each 10 knot reduction in speed. From 150 to 110 knots it needs

  • A.2.5 degrees
  • B.10 degrees up
  • C.4 degrees
  • D.25 degrees

Answer: B

Correct answer: 10 degrees up

The speed change is 40 knots, which is four increments of 10:

\[ \frac{150 - 110}{10} \times 2.5 = 4 \times 2.5 = 10^\circ \]

The deflection is up, since slower flight needs a higher angle of attack and therefore more download at the tail. The relation is treated as linear here, which is a fair approximation over a modest speed range; across the whole envelope the elevator-against-speed curve is distinctly non-linear.

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