21-02. AIRFRAME
All questions: 38
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Questions for exams: 25
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1. In flight, a cantilever wing of an airplane containing fuel undergoes vertical loads which produce a bending moment:
2. How can in flight wing loading be reduced?
3. With reference to stringers they:
4. On a non-stressed skin type wing, the wing structure elements which take up the vertical bending moments Mx are:
5. What mission does the strut have, often observed between the fuselage and the wing, on small high wing aircraft?
