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Panting fatigue of AL-6XN stainless ...

Paterson, Duncan.

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Panting fatigue of AL-6XN stainless steel box girders.

紀錄類型:	書目-電子資源 : Monograph/item
正題名/作者:	Panting fatigue of AL-6XN stainless steel box girders./
作者:	Paterson, Duncan.
面頁冊數:	361 p.
附註:	Source: Dissertation Abstracts International, Volume: 65-03, Section: B, page: 1450.
Contained By:	Dissertation Abstracts International65-03B.
標題:	Engineering, Civil. -
電子資源:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3127532
ISBN:	0496747967

Panting fatigue of AL-6XN stainless steel box girders.
Paterson, Duncan.

Panting fatigue of AL-6XN stainless steel box girders. - 361 p.

Source: Dissertation Abstracts International, Volume: 65-03, Section: B, page: 1450.

Thesis (Ph.D.)--Lehigh University, 2004.

Three large scale single cell box girders and two triple cell box girders of AL-6XN superaustenitic stainless steel simulating components of double hull ship structures were tested under repeated reversal bending of constant magnitude for examining fatigue behavior of such components. The flange and web plates of the boxes deflected repeatedly out-of-plane (panting). Local stress ranges along the boundaries of flange plate panels were much higher than the nominal stress ranges and fatigue cracks developed at these locations of higher stress ranges. The fatigue strength category in terms of S-N curve is, therefore, lower than that for plate panels without out-of-plane deflection.

ISBN: 0496747967Subjects--Topical Terms:

783781
Engineering, Civil.

Panting fatigue of AL-6XN stainless steel box girders.
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100 1 $a Paterson, Duncan. $3 1936719
245 1 0 $a Panting fatigue of AL-6XN stainless steel box girders.
300 $a 361 p.
500 $a Source: Dissertation Abstracts International, Volume: 65-03, Section: B, page: 1450.
500 $a Adviser: Ben T. Yen.
502 $a Thesis (Ph.D.)--Lehigh University, 2004.
520 $a Three large scale single cell box girders and two triple cell box girders of AL-6XN superaustenitic stainless steel simulating components of double hull ship structures were tested under repeated reversal bending of constant magnitude for examining fatigue behavior of such components. The flange and web plates of the boxes deflected repeatedly out-of-plane (panting). Local stress ranges along the boundaries of flange plate panels were much higher than the nominal stress ranges and fatigue cracks developed at these locations of higher stress ranges. The fatigue strength category in terms of S-N curve is, therefore, lower than that for plate panels without out-of-plane deflection.
520 $a The experimental study is supplemented with a parametric finite element study. The results of the finite element study indicate that the local maximum stress range of an edge loaded plate with initial out-of-flatness can be predicted. With this knowledge and using the ASSHTO fatigue design curves, certain parameters, such as the slenderness ratio can be limited or adjusted to control fatigue damage.
590 $a School code: 0105.
650 4 $a Engineering, Civil. $3 783781
650 4 $a Engineering, Mechanical. $3 783786
650 4 $a Applied Mechanics. $3 1018410
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690 $a 0548
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710 2 0 $a Lehigh University. $3 515436
773 0 $t Dissertation Abstracts International $g 65-03B.
790 1 0 $a Yen, Ben T., $e advisor
790 $a 0105
791 $a Ph.D.
792 $a 2004
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=3127532