SI: Showcasing Structural Integrity Research in India
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Vol. 13, No. 48 (2019) pp. 630-638
Effect of Contact Geometry on the Contact Stresses in a Flat with Round Edge Contact
The blade-disc dovetail interface in an aero-engine compressor is characterized by a non-uniform pressure distribution which can be obtained by an equivalent flat with round edge-on-plate configuration. The contact tractions for a mating…