Sentence examples for fastened design from inspiring English sources

Exact(1)

It is shown that the design strengths predicted by the North American Specification using the unfastened design rules are generally conservative, but unconservatively predicted using the fastened design rules, even when the flanges of the specimens were restrained.

Similar(59)

In view of the close fit, the models with solid railpads can be used for track and fastening design and to derive track parameters to, for instance, study the deterioration of tracks.

This fastens the design of metabolic circuits using a combinatorial design approach, where given pathways could be optimized for maximal bioproduction, while being nontoxic for the chassis.

The engineered fastening business primarily sells engineered fasteners designed for specific applications.

Fastener failure thus requires special consideration in designing crashworthy fastened composite structures; if it can be delayed, energy absorption is greater.

Comparison of experimental shear capacities with corresponding predictions from the current Australian cold-formed steel design rules showed that the current design rules are very conservative for the shear design of rivet fastened RHFCBs.

Leave it to the Europeans to treat the shirtdress subversively, as did Jean Paul Gaultier, whose sheeting-crisp cotton poplin version for Hermès ($1,975), shown here in several guises, has sexily bunched bracelet sleeves and buttons that veer off course by design, fastening provocatively somewhere to the left of center.

Improved design rules were proposed for rivet fastened RHFCBs based on the current shear design equations in AISI S100 and the direct strength method.

This paper presents a literature review of the state-of-the-art experimental and analytical methodologies adopted in the construction industry for the design of mechanically fastened connections and joints in pultruded fibre reinforced polymer framed structures.

Issues related to design of mechanically fastened joints in composite aircraft fuselage structures are studied, such as the effects of joint thickness, laminate taper (i.e. the positioning of the plies in the taper region) and secondary bending on joint stiffness and strength.

Both experiments and model have shown that the composite FTB is capable to effectively carry the load which the original fastened metallic FTB has been designed to carry.

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