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Published June 8, 2004 | public
Journal Article

A fast algorithm for the simulation of polycrystalline misfits. II. Martensitic transformations in three space dimensions

Abstract

We present a fast numerical method for the simulation of martensitic transformations in three–dimensional polycrystals. To produce the relevant overall elastic energy arising from given boundary conditions, this method proceeds by reducing the corresponding non–convex minimization problem to minimization of a certain quadratic form—over the set of arrays of transformation strains which are compatible with a given distribution of crystallite orientations. The evaluation of this quadratic form for a given array of transformation strains requires solution of certain linear elasticity problems. An acceleration strategy we use, which for a polycrystal containing N grains reduces the complexity of the algorithm from O(N^2) to O(N) operations, results from a formulation of the minimization problem which takes advantage of certain decorrelations present in the minimizing arrays of transformation strains. We illustrate our presentation with a number of examples involving cubic–to–monoclinic and cubic–to–orthorhombic polycrystalline phase transitions, such as those arising in the TiNi and CuAl shape–memory alloys. In particular, our study quantifies the effects of texture on the overall properties of such polycrystalline shape–memory alloys.

Additional Information

© 2004 The Royal Society. Received 24 April 2003; accepted 11 August 2003; published online 9 March 2004. This work was sponsored by the Air Force Office of Scientific Research, Air Force Materials Command, USAF, under grant numbers F49620-96-1-0008 and F49620-99-1-0010. The authors gratefully acknowledge support from NSF (through an NYI award). O.P.B. gratefully acknowledges support from NSF (through contract numbers DMS-9523292 and DMS-9816802) and from the Powell Research Foundation. The US Government is authorized to reproduce and distribute reprints for governmental purposes notwithstanding any copyright notation thereon. The views and conclusions contained herein are those of the authors and should not be interpreted as necessarily representing the official policies or endorsements, either expressed or implied, of the Air Force Office of Scientific Research or the US Government.

Additional details

Created:
August 22, 2023
Modified:
October 25, 2023