Mathematical Problems in Engineering / 2011 / Article / Tab 3

Research Article

A Corotational Finite Element Method Combined with Floating Frame Method for Large Steady-State Deformation and Free Vibration Analysis of a Rotating-Inclined Beam

Table 3

Comparison of results for different cases ( πœ‚ = 1 0 0 0 , 𝑅 = 1 . 5 ).

𝛼 π‘˜   πœ€ 𝑐 m a x
( 1 0 βˆ’ 3 )
πœ€ 𝑏 m a x
( 1 0 βˆ’ 3 )
𝑣 t i p / 𝐿 𝑇 𝐾 1
( 1 0 βˆ’ 2 )
𝐾 2
( 1 0 βˆ’ 1 )
𝐾 3
( 1 0 βˆ’ 1 )
𝐾 4 𝐾 5 𝐾 6 𝐾 7

EA10000.351601.220349.617105.121008.200340.300117.421052
EA50000.351601.220341.616949.120893.199838.298509.416903
0EA100000.351601.220341.616948.120893.199837.298506.416896
[24]000.352.2203.6169.12089.19984.29851β€”
0Β°[34]000.3516.22034.616972.120902β€”β€”β€”
EA106.93309009.004572.501864.13423.591446.784725.9929271.21760
EA507.15492008.962392.474244.06068.580524.771309.9761201.19365
0.06EA1007.18210008.961522.473124.05756.580088.770833.9756341.19316
[24]7.20000008.9522.47084.0536.57955.77017.97486β€”
LAS7.2000000β€”β€”β€”β€”β€”β€”β€”

EA101.731133.88303.08351714.547141.274482.17658.323098.443024.577262.726698
5Β°0.03EA501.783966.00526.08381944.533481.262202.15028.319777.439167.572464.719965
EA1001.789366.20203.08382184.533201.261792.14942.319678.439068.572368.719873
LAS1.79486101.89714.70753β€”β€”β€”β€”β€”β€”β€”

EA10.1171748.73588.4296881.29068.405580.836390.143462.221484.319586.439110
30Β°0.008EA50.1143419.36150.4299791.28848.404156.836065.143631.221433.318254.434653
EA100.1134109.38784.4299861.28840.404108.836056.143643.221458.318289.434691
LAS.11513841.56926.00000β€”β€”β€”β€”β€”β€”β€”

EA10006325878.11012.747138.561367.232168.566051.113317.190889.289637.409722
90Β°0.003EA50003882248.15298.747250.560585.232182.566299.113204.190326.287895.405359
EA100.003517408.15396.747254.560558.232181.566306.113202.190322.287886.405342
LAS.0045000011.69131.68750β€”β€”β€”β€”β€”β€”β€”