Anisotropic elasticity by Ting T.C.T.

By Ting T.C.T.

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Engng. 23 (1985) pp. 1547-1565. C. : "Dynamic Analysis of Embedded Rigid Strip Footings by Time Domain Boundary Element Method", Proc. 7th. Int . Conf. A. ) voI. I (1985) pp. 6-71 to 6-78. J. : "A Time-Stepping Technique to Solve Wave Propagation Problems Using the Boundary Element Method", Ph, D. Thesis, Southarnpton Unive rsity 1983. : "A Boundary Element Procedure for Transient Wave Propagation in Two-Dimensional Isotropic Elastic Media", Finite Elements in Analysis and Design 1 (1985), pp. 313-322.

In this part of the method an a ut oma t i c procedure for generating a (curvature- or even solution-)adaptive panelling would re sult in an increased accuracy . AIC : In this part of the program the influence integrals are evaluated, the operational count i s 0(N 2 ) . In present-day panel methods, using an iterative solver for the system of equations, this part of the program accounts for up to 80% of the tot al CPU time. Here attention has t o be paid to the vect orizat ion of the code , su ch that it runs ef ficiently on super-computers.

J. : "The supers onic triplet - A new aerodynamic panel singui arity with di rectional properties", AIAA J ou r na l , Volo 18, No. 2 (1980), pp. 138-14 2 . , Rubbe r t , P. E. : "A co mpar ison of pa ne L me t hods fo r subs on ic f I ow c omput at i on", AGARDog raph No. 241 (19 79). : "Asymptotic convergence of h igher-order accurate panei methods", J. of Aircraft, Volo 23 , No. 2 (1986), pp. 126-130. , Hewitt, B. : "The ind irect boundary-integral formul ation for ellipt ic, hy pe rbo lic a nd non- linear fl ui d f I ows " , Ch .

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