FIFTH SEMESTER B.E AERONAUTICAL ENGINEERING-AIRCRAFT STRUCTURES II

FIFTH SEMESTER – B.E – AERONAUTICAL ENGINEERING
12AE2503 – AIRCRAFT STRUCTURES -II

Answer ALL questions
Duration: 3 Hours Maximum: 100 Marks
PART – A (10 x 1 = 10 Marks)

1. The bending moment on a section is maximum where shear force is
a) minimum b) maximum c) changing sign d) zero

2. An example for single axis symmetry is
a) Right angled triangle b) Trapezoidal section c) Circular section d) Angle section

3. When the force applied to shear centre
a) Bending only occur b) Twisting only occur
c) Bending and twisting occur d) No bending and no twisting

 

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