Propose conceptual design for wing of twin gas-turbine


Problem: As an aeronautical engineer, your first job is to propose a conceptual design for the wing of a twin gas-turbine-engine powered aircraft for commercial purposes.

(a) Suggest ONE (1) desirable design for the aircraft wing to maintain stability in ALL three axes.

(b) Sketch the free body diagram of desirable wing design and state your reasons.

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Mechanical Engineering: Propose conceptual design for wing of twin gas-turbine
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