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研究生:謝全釗
研究生(外文):Shieh, Chyuan Jau
論文名稱:複材疊層板接觸行為之研究
論文名稱(外文):The Contact Behavior of Composite Laminate
指導教授:陳文華陳文華引用關係
指導教授(外文):Chen, Wen Hwa
學位類別:碩士
校院名稱:國立清華大學
系所名稱:動力機械學系
學門:工程學門
學類:機械工程學類
論文種類:學術論文
論文出版年:1994
畢業學年度:82
語文別:中文
論文頁數:61
中文關鍵詞:複材疊層板接觸
外文關鍵詞:composite laminatecontact
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本論文主要發展複合式應力有限單元分析模式,配合接觸力學分析程序,
研究複材疊層板與剛性球體間三維無摩擦接觸問題。由於複合式應力有限
單元分析中,未知參數和自由度均與層數無關,且接觸面滿足幾何諧合條
件,適合用以處理複材疊層板與剛性球體間三維無摩擦接觸問題。經由實
例解析,證實了本分析方法的正確性與適用性。對於疊層效應,球體直徑
效應,跨距效應及邊界效應對凹陷律的影響,亦做詳細的探討。

A hybrid stress multilayer element model together with the
contact mechanics analysis procedure are developed to study the
three dimensional frictionless contact problem between a
general composite laminate and a rigid sphere. The multilayer
element model is formulated based on a modefied complementary
energy priciple. To relax the equilibrium of interelement
tractions, in addition to the stress field in the interior of
the element, the Lagrangian multipliers which are physically
the interelement boundary displacements are introduced and the
interelement traction reciprocity and mechanical boundary
conditions are satisfied. Besides, in the multilayer elements
model, the undetermined stress parameters and total degrees of
freedom are independent of the number of layers and the
kinematic conditions are satisfied on the ntact surfaces.
Hence, the application of the present techique has no limiation
of the geometry, stacking arrangement , boundary conditions and
number of layers. The contact problem of a general graphite/
epoxy laminate and a rigid sphere is solved. Excellent
agreements between the present result andference solutions show
the high accuracy and validity of the technique developed. The
effects of sphere diamenter, stacking arrangement, span and
boundary conditions on the indentation law are also disscussed
in details.

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