Example 19.1 Determine the direct stress distribution in the wing section shown in Fig. 192 when it is subjected to a be
Posted: Sat May 21, 2022 10:36 am
Example 19.1 Determine the direct stress distribution in the wing section shown in Fig. 192 when it is subjected to a bending moment of 5,000 Nm applied in a vertical plane. 50 50 I-