Proceedings of the ... International Conference on Offshore Mechanics and Arctic Engineering, Volume 9American Society of Mechanical Engineers, 1990 - Arctic regions |
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Page 272
... factor , defined below , is constant as long as the pre - load is in force . Kid Ktd = ᎪᏢ ASP = 1.65 connection with pre - load ( 7 ) = Δσο = 5.4 connection without pre - load AS ( 8 ) It is also apparent that the dynamic stress ...
... factor , defined below , is constant as long as the pre - load is in force . Kid Ktd = ᎪᏢ ASP = 1.65 connection with pre - load ( 7 ) = Δσο = 5.4 connection without pre - load AS ( 8 ) It is also apparent that the dynamic stress ...
Page 279
... factor KTH and then combined with the factor Kp due to thread bending using Heywood's formula , below which accounts for KTH and KB not being coincident on the thread root : K + = KB + where : Kih 1 + C ( KB / Kth ) [ 13 ] C is an ...
... factor KTH and then combined with the factor Kp due to thread bending using Heywood's formula , below which accounts for KTH and KB not being coincident on the thread root : K + = KB + where : Kih 1 + C ( KB / Kth ) [ 13 ] C is an ...
Page 356
... factor F .. Based on fatigue tests , Raju and Newman ( 1981 ) have estimated this factor F , 0.9 . But in the case of surface crack growth , m.m. and C.-C. , thus the factor F , should be equal to 1.0 . 3.3 . Stress Intensity Factor The ...
... factor F .. Based on fatigue tests , Raju and Newman ( 1981 ) have estimated this factor F , 0.9 . But in the case of surface crack growth , m.m. and C.-C. , thus the factor F , should be equal to 1.0 . 3.3 . Stress Intensity Factor The ...
Contents
ADVANCED COMPOSITES | 1 |
Probabilistic Aspects of HAZ CTOD Value of Multipass Welded Joint of Steel for Offshore | 5 |
The Use of GRP Materials in Platform Topsides Construction and the Regulatory Implications | 15 |
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analysis applications axial behaviour bending brace calculated carried chord combined compared components composite Composite Materials compression concrete connection considered construction corrosion crack crack growth critical curve cycles damage determined developed distribution effect element Engineering experimental factor failure fatigue fiber Figure finite element force fracture geometry increase indicate initial internal laminate length limit load lower Marine material matrix maximum mean measured mechanical method Mode nodes nominal normal observed obtained offshore operation parameters performance pipe plate platform position predicted present pressure production properties range ratio reduced reinforcement Research resin resistance seal shear shell shown shows specimen steel stiffener stiffness strain strength stress concentration structures surface Table techniques temperature tensile tension thickness thread tube tubular joints weight weld