-element bar -400 cm c 0, and simply suppor subject to flexura expressed as a function of the material density p, the cross-sectional area is A, the second moment of area I, and the Young's modulus, E, as: ΕΙ @²=b- PA Answer the following: • The number of degrees of freedom of the bar is The value of b is . The units of b are (give your answer to 2 decimal places) (in the international system, SI) Note local mass and stiffness matrices for bars subject to flexural vibrations are given here: 12 6L -12 6L 6L 4L² -6L 2L² -12 -6L 12 -6L 6L 2L² -6L 4L² M= 22L 54 -13L 4L² 13L -3L² 54 13L 156 -22L -13L-3L² -22L 4L² 156 PAL 22L 420 and K= tion. Its square natural frequency can ΕΙ L3

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
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A one-element bar of length L=400 cm clamped at x=0, and simply supported at x=l. The bar is subject to flexural vibration. Its squared natural frequency can be
expressed as a function of the material density p, the cross-sectional area is A, the second moment of area I, and the Young's modulus, E, as:
ΕΙ
@²=b-
PA
Answer the following:
• The number of degrees of freedom of the bar is
The value of b is
. The units of b are
(give your answer to 2 decimal places)
(in the international system, SI)
Note local mass and stiffness matrices for bars subject to flexural vibrations are given here:
156 22L
54 -13L
4L² 13L -3L²
54 13L 156 -22L
-13L-3L² -22L 4L²
M=
PAL 22L
420
and K =
ΕΙ
L³
12 6L -12 6L
6L 4L2 -6L 2L²
-12 -6L 12 -6L
6L 2L² -6L 4L²
Transcribed Image Text:A one-element bar of length L=400 cm clamped at x=0, and simply supported at x=l. The bar is subject to flexural vibration. Its squared natural frequency can be expressed as a function of the material density p, the cross-sectional area is A, the second moment of area I, and the Young's modulus, E, as: ΕΙ @²=b- PA Answer the following: • The number of degrees of freedom of the bar is The value of b is . The units of b are (give your answer to 2 decimal places) (in the international system, SI) Note local mass and stiffness matrices for bars subject to flexural vibrations are given here: 156 22L 54 -13L 4L² 13L -3L² 54 13L 156 -22L -13L-3L² -22L 4L² M= PAL 22L 420 and K = ΕΙ L³ 12 6L -12 6L 6L 4L2 -6L 2L² -12 -6L 12 -6L 6L 2L² -6L 4L²
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