Buckling and initial postbuckling behavior is determined for thin, elastic cylindrical shells of elliptical cross section. This study complements the buckling and advanced postbuckling calculations reported by Kempner and Chen on a similar class of shells. The initial postbuckling analysis indicates that, like compressed circular cylinders, the oval cylinders will be highly sensitive to small geometrical imperfections and may buckle at loads well below the predictions for the perfect shell. On the other hand, buckling will not necessarily result in complete collapse. A series of simple tests has been performed which provide qualitative verification of the major features of the theory.
Abstract Attention deficit hyperactivity disorder (ADHD) is a highly heritable disorder affecting some 5–10% of children and 4–5% of adults. The cannabinoid receptor gene ( CNR1 ) is a positional candidate gene due to its location near an identified ADHD linkage peak on chromosome 6, its role in stress and dopamine regulation, its association with other psychiatric disorders that co‐occur with ADHD, and its function in learning and memory. We tested SNP variants at the CNR1 gene in two independent samples—an unselected adolescent sample from Northern Finland, and a family‐based sample of trios (an ADHD child and their parents). In addition to using the trios for association study, the parents (with and without ADHD) were used as an additional case/control sample of adults for association tests. ADHD and its co‐morbid psychiatric disorders were examined. A significant association was detected for a SNP haplotype (C‐G) with ADHD ( P = 0.008). A sex by genotype interaction was observed as well with this haplotype posing a greater risk in males than females. An association of an alternative SNP haplotype in this gene was found for post‐traumatic stress disorder (PTSD) ( P = 0.04 for C‐A, and P = 0.01 for C‐G). These observations require replication, however, they suggest that the CNR1 gene may be a risk factor for ADHD and possibly PTSD, and that this gene warrants further investigation for a role in neuropsychiatric disorders. © 2008 Wiley‐Liss, Inc.
As preparation for a workshop on Dynamics of Fault Zones (95 th Dahlem Workshop, Berlin, January 2005), specifically on the sub-topic Rheology of Fault Rocks and Their Surroundings, we addressed critical research issues for understanding the seismic response of fault zones in terms of the constitutive response of fault materials. That requires new concepts and a host of new observations and experiments to document material response, to understand the shear localization process and the inception of earthquake instability, and especially to understand the mechanisms of fault weakening and dynamics of rupture tip propagation and arrest during rapid, possibly large, slip in natural events. We examine in turn the geological structure of fault zones and its relation to earthquake dynamics, the description of rate and state friction at slow rates appropriate to the interseismic period and earthquake nucleation, and the dynamics of fault weakening during rapid slip. The last topic gets special attention here in view of the important recent advances in theoretical concepts and experiments to probe the range of slip rates prevailing during earthquakes. We then address the assembly of the constitutive framework into viable but necessarily simplified conceptual and computational models for description of the dynamics of crustal earthquake rupture. This is done principally in the slipweakening framework, and we examine some of the uncertainties in doing so, and issues of how new understanding of the rapid large slip range will be integrated to model the traction evolution and the weakening process during large slip episodes.
Argues that new military aircraft will benefit from a fuel control system that is technically superior to that of the present day, and is also geared to match the yet‐to‐be‐introduced maritime patrol aircraft, Nimrod 2000's aircraft‐engine combination. Charts the case of RoSEC, a company formed in 1993 to provide complete full‐authority digital engine control systems. Claims that the new “total responsibility” approach will bring significant fuel system advantages in the commercial and military aerospace sector.