The 3D-computer cluster simulation of forming the large-sized one-piece airframe panels with bicurvature and variable thickness


  • M.A. Guzev Presidium of Far East Branch of the Russian Academy of Sciences (FEB RAS)
  • A.I. Oleinikov Komsomolsk-on-Amur State University
  • K.S. Bormotin Komsomolsk-on-Amur State University
  • S.V. Seriy Komsomolsk-on-Amur State University
  • A.I. Pekarsh KnAAZ - Branch of PJSC «Company «Sukhoi»


вычислительные кластеры, метод конечных элементов, развертка, формовка, ползучесть, оснастка, проектирование крыльевых панелей


Problems of high-performance computer simulation and refining the technological regimes of forming airframe panels and calculation of their parts are considered. Some numerical results of using FEM-computations obtained on the MVS-1000 supercomputer and on a cluster of standard PCs are given. An algorithm designed for stress calculation with consideration of the material heteroresistance is applied. Simulation data are compared with small-scale and full-scale experiments. Computing efficiency of clusters with various number of nodes is estimated. This work was supported by the Russian Foundation for Basic Research (projects 07-01-00747, 06-II-СО-01-002, NS-9004.2006.1). The paper was prepared on the basis of the author’s report at the International Conference on Parallel Computing Technologies (PaVT-2007;

Author Biographies

M.A. Guzev

A.I. Oleinikov

K.S. Bormotin

S.V. Seriy

A.I. Pekarsh


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  2. Савяк В. Эффективные кластерные решения (
  3. Олейников А.И. Об описании деформирования гетерогенно-сопротивляющихся материалов // Докл. РАН. 1998. 361, № 6. 773-774.



How to Cite

Гузев М., Олейников А., Бормотин К., Серый С., Пекарш А. The 3D-Computer Cluster Simulation of Forming the Large-Sized One-Piece Airframe Panels With Bicurvature and Variable Thickness // Numerical Methods and Programming (Vychislitel’nye Metody i Programmirovanie). 2007. 8. 123-129



Section 1. Numerical methods and applications

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