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Hydraulic system affect conceptual design based on __________

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in Aircraft Design by (701k points)
Hydraulic system affect conceptual design based on __________

(a) hydraulic pump space requirements

(b) space for control surface

(c) secondary control surface

(d) lift required at tail

The question was asked during an interview.

The origin of the question is Subsystems topic in portion Landing Gear and Subsystems of Aircraft Design

1 Answer

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Best answer
Correct choice is (a) hydraulic pump space requirements

For explanation: A typical hydraulic system will affect conceptual design based on space requirements for pumps typically. Control surface are located at the wing or at tail section. Lift required at tail will be affected by which type of airfoil is used.

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