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Figure Q6 shows the cantilevered 6061-T6 aluminum alloy rectangular beam fixed at A. Given Modulus Rigidity, G 26 GPa and Young Modulus, E = 68.9XGPA (a) Construct the internal loadings (FBD) and shows the value of internal loadings.

Figure Q6 shows the cantilevered 6061-T6 aluminum alloy rectangular beam fixed at A. Given Modulus Rigidity, G 26 GPa and Young Modulus, E = 68.9XGPA (a) Construct the internal loadings (FBD) and shows the value of internal loadings.

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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300 kN 2 m 200 mm 600 mm A La Section a - a
Transcribed Image Text:300 kN 2 m 200 mm 600 mm A La Section a - a
Figure Q6 shows the cantilevered 6061-T6 aluminum alloy rectangular beam fixed at A. Given Modulus Rigidity, G 26 GPa and Young Modulus, E = 68.9×GPA (a) Construct the internal loadings (FBD) and shows the value of internal loadings. (b) (c) (d)
Transcribed Image Text:Figure Q6 shows the cantilevered 6061-T6 aluminum alloy rectangular beam fixed at A. Given Modulus Rigidity, G 26 GPa and Young Modulus, E = 68.9×GPA (a) Construct the internal loadings (FBD) and shows the value of internal loadings. (b) (c) (d)
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