Q.05. Under cruising conditions the distributed load acting on the wing of a small airplane has the idealized variation shown in the figure. Calculate and draw the shear force V and bending moment M...


Q.05. Under cruising conditions the distributed load acting on the wing of a small airplane has the<br>idealized variation shown in the figure. Calculate and draw the shear force V and bending moment<br>M at the inboard end of the wing.<br>-1600 N/m<br>900 N/m<br>1.0 m<br>- 2.6 m<br>- 2.6 m -<br>

Extracted text: Q.05. Under cruising conditions the distributed load acting on the wing of a small airplane has the idealized variation shown in the figure. Calculate and draw the shear force V and bending moment M at the inboard end of the wing. -1600 N/m 900 N/m 1.0 m - 2.6 m - 2.6 m -

Jun 11, 2022
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