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Bevelled adherend

Beveled lap joints. These joints are also more efficient than plain lap joints. The beveled edges allow conformance of the adherends during loading, with a resultant reduction of cleavage stress at the ends of the joint. [Pg.167]

Fig. 3. (a) By rotating the coordinate reference frame, normal stresses and shear stresses vary, obeying Mohr s circle, a graphical transformation technique for analyzing second-order tensors. Here are illustrations for uniaxial tension and pure shear, (b) Illustration of how average normal and shear stresses across a bondline vary with angle in a beveled joint. Results are normalized with respect to the nominal stress, oo = PI Ao, the load divided by the cross-sectional area of the adherends. [Pg.9]

THE EFFECT OF ADHEREND SHAPE—SCARFED, BEVELLED AND STEPPED ADHERENDS... [Pg.69]

It may be useful to the reader to consider as an example the work by Adams et al (1978c) and some of their hitherto unpublished results. They used finite-element methods to examine the stresses in high-performance composites in symmetrical lap joints with parallel, bevelled, scarfed and stepped adherends. The composite adherends were assumed to be linearly elastic type II carbon fibre reinforced epoxy composites with a 60% fibre volume fraction. The mechanical properties of this material are given in Table 3. [Pg.74]


See other pages where Bevelled adherend is mentioned: [Pg.268]    [Pg.167]    [Pg.438]    [Pg.438]    [Pg.769]    [Pg.769]    [Pg.299]    [Pg.299]    [Pg.300]    [Pg.416]    [Pg.27]    [Pg.70]    [Pg.104]    [Pg.191]    [Pg.551]   
See also in sourсe #XX -- [ Pg.69 , Pg.70 , Pg.71 ]




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