Mathematical Problems in Engineering / 2011 / Article / Tab 2

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 2

Comparison of results for different cases ( πœ‚ = 2 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
( 1 0 βˆ’ 3 )
𝐾 1 𝐾 2 𝐾 3 ( π‘Ž ) 𝐾 4 𝐾 5 ( π‘Ž ) 𝐾 6 𝐾 7 ( π‘Ž )

EA10000.1747881.059571.572412.824954.756105.195468.00214
EA50000.1747871.059531.570862.824314.714135.191207.86206
0EA100000.1747871.059531.570812.824314.712835.191197.85600
[24]000.174791.059531.570802.824314.712395.19119β€”
0Β°[34]000.175801.101721.570803.084864.712396.04510β€”
EA106.9330900.1986161.087561.576152.853334.757295.223848.02928
EA507.1549200.1985141.087261.576162.852434.715345.219317.86274
0.06EA1007.1821000.1985111.087261.574572.852424.714035.219307.85669
[24]7.2000000.198621.087601.574552.852764.713605.21962β€”
LAS7.2000000β€”β€”β€”β€”β€”β€”β€”

EA101.726801.930985.47630.1810491.066611.573352.832064.756395.202568.00889
5Β°0.03EA501.781951.935465.47699.1810211.066511.571802.831364.714435.198237.86221
EA1001.788701.935605.47701.1810201.066511.571752.831364.713125.198227.85616
LAS1.794862.037945.88301β€”β€”β€”β€”β€”β€”β€”

EA10.1732981.290083.72294.1754101.060281.572522.825674.756135.196198.00281
30Β°0.01EA50.1786151.292243.72299.1754071.060241.570972.825034.714165.191917.86207
EA100.1792641.292313.72300.1754071.060241.570922.825034.712855.191907.85601
LAS.1799041.299043.75000β€”β€”β€”β€”β€”β€”β€”

EA10.05003452.593647.49504.1748361.059781.572532.825204.756125.195738.00229
90Β°0.01EA50.05003842.597847.49506.1748351.059741.570982.824564.714155.191457.86205
EA100.05002162.597977.49507.1748351.059741.570932.824564.712845.191447.85599
LAS.05000002.598077.50000β€”β€”β€”β€”β€”β€”β€”