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School of Computer Science

Tel-Aviv Academic College

Prof. Boris Epstein memory candle

Prof. Boris Epstein

November 17, 1947 — July 1, 2020

memory candle

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Journal/Collection Publications

50 S. Peigin, S. Timchenko and B. Epstein. The Stability of the Optimal Aerodynamic Design of an Isolated Three-Dimensional Wing to Its Initial Form, Technical Physics, volume 63, pages 1736–1742, December 2018.
49 Boris Epstein and Sergey Peigin. Automatic optimization of wing–body–under-the-wing-mounted-nacelle configurations, Journal of Aircraft, volume 53, number 3, pages 691–700, American Institute of Aeronautics and Astronautics, May 2016.
48 Sergey Peigin and Boris Epstein. Automatic Design of Wing–Body–Nacelle Configurations for Minimum Drag, AIAA Journal, volume 53, number 7, pages 1994–2004, American Institute of Aeronautics and Astronautics, July 2015.
47 Sergey PEIGIN, 朱自强 Zhu Ziqiang and Boris EPSTEIN. 可应用于民机空气动力设计中的数值优化方法 Numerical optimization method applicable to civil aircraft aerodynamic design, 航空学报 (Journal of Aviation), pages 58–69, 2014.
46 C. Popovich, N. Shapiro, B. Epstein and S. Peigin. Massively Parallel Industry-strength Design of Aerodynamic Wings, Procedia Engineering, volume 61, pages 292—297, 2013, 25th International Conference on Parallel Computational Fluid Dynamics.
45 S. Peigin and B. Epstein. Massive Parallelization for industrial CFD based analysis and design, in P. Iványi and B.H.V. Topping (eds.), Trends in Parallel, Distributed, Grid and Cloud Computing in Engineering, Computational Science, Engineering and Technology Series, volume 27, pages 269–290, Saxe-Coburg Publications, 2011.
44 S. Peigin, B. Epstein and S. Gali. Parallel implementation of fictitious surfaces method for aerodynamic shape optimization, in Lecture notes in computational science and engineering, volume 74, pages 71–82, Springer, 2010.
43 Boris Epstein and Sergey Peigin. Treatment of nonmatched grids for high-accuracy Navier-Stokes solutions, AIAA journal, volume 48, number 7, pages 1542–1553, July 2010.
42 Boris Epstein, Antony Jameson, Sergey Peigin, Dino Roman, Neal Harrison and John Vassberg. Comparative study of three-dimensional wing drag minimization by different optimization techniques, Journal of Aircraft, volume 46, number 2, pages 526–541, 2009.
41 藍庭顯, 黃翔瑜 and 許彥文. 應用基因演算法求 NACA0012 翼剖面最大升阻比之探討, Journal of China Institute of Technology, volume 40, 2009.
40 Boris Epstein and Sergey Peigin. ACCURATE INCORPORATION OF NON-TO-POINT MATCHED COMPUTATIONAL BLOCKS INTO FULL NAVIER-STOKES COMPUTATIONS ON STRUCTURED GRIDS, 2008.
39 Sergey Peigin and Boris Epstein. Multiconstrained aerodynamic design of business jet by CFD driven optimization tool, Aerospace Science and Technology, volume 12, number 2, pages 125–134, Elsevier, 2008.
38 Sergey Peigin and Boris Epstein. Aerodynamic optimization of essentially three-dimensional shapes for wing-body fairing, AIAA journal, volume 46, number 7, pages 1814–1825, 2008.
37 Boris Epstein and Sergey Peigin. HYBRIDIZATION OF HETEROGENEOUS 3D CFD DISCRETIZATIONS VIA DIRECT FLUX OPTIMIZATION, September 2008.
36 Boris Epstein and Sergey Peigin. Efficient approach for multipoint aerodynamic wing design of business jet aircraft, AIAA journal, volume 45, number 11, pages 2612–2621, 2007.
35 Sergey Peigin and Boris Epstein. Multipoint aerodynamic design of wing-body configurations for minimum drag, Journal of aircraft, volume 44, number 3, pages 971–980, 2007.
34 Boris Epstein and Sergey Peigin. Accurate CFD driven optimization of lifting surfaces for wing-body configuration, Computers & fluids, volume 36, number 9, pages 1399–1414, Elsevier, January 2007.
33 Amir Averbuch, Boris Epstein, Neta Rabin and Eli Turkel. Edge-enhancement postprocessing using artificial dissipation, IEEE transactions on image processing, volume 15, number 6, pages 1486–1498, IEEE, 2006.
32 Boris Epstein, Sergey Peigin and Shlomo Tsach. A new efficient technology of aerodynamic design based on CFD driven optimization, Aerospace science and technology, volume 10, number 2, pages 100–110, Elsevier, 2006.
31 Sergey Peigin and Boris Epstein. Optimization of Blended Wing Body Aircraft by Automatic CFD Driven Design Tool, 2006.
30 Sergey Peigin and Boris Epstein. Computational fluid dynamics driven optimization of blended wing body aircraft, AIAA journal, volume 44, number 11, pages 2736–2745, 2006.
29 Sergey Peigin and Boris Epstein. Robust drag minimization of aerodynamic wings in engineering environment, Journal of aircraft, volume 43, number 4, pages 1195–1204, 2006.
28 Boris Epstein and Sergey Peigin. Constrained aerodynamic optimization of three-dimensional wings driven by Navier-Stokes computations, AIAA journal, volume 43, number 9, pages 1946–1957, 2005.
27 Stephane Séror, Theodor Rubin, Sergey Peigin and Boris Epstein. Implementation and validation of the Spalart-Allmaras turbulence model in parallel environment, Journal of aircraft, volume 42, number 1, pages 179–188, 2005.
26 Elena Braverman, Boris Epstein, Moshe Israeli and Amir Averbuch. A fast spectral subtractional solver for elliptic equations, Journal of Scientific Computing, volume 21, pages 91–128, Springer, 2004.
25 Boris Epstein and Sergey Peigin. Robust hybrid approach to multiobjective constrained optimization in aerodynamics, AIAA journal, volume 42, number 8, pages 1572–1581, 2004.
24 S Peigin and Boris Epstein. Embedded parallelization approach for optimization in aerodynamic design, The Journal of Supercomputing, volume 29, number 3, pages 243–263, Springer, 2004.
23 Sergey Peigin and Boris Epstein. Robust optimization of 2D airfoils driven by full Navier–Stokes computations, Computers & fluids, volume 33, number 9, pages 1175–1200, Elsevier, 2004.
22 S. Peigin, B. Epstein and S. Gali. - Multilevel parallelization strategy for optimization of aerodynamic shapes, in A. Ecer, N. Satofuka, J. Periaux and P. Fox (eds.), Parallel Computational Fluid Dynamics 2003, pages 505—512, Elsevier, 2004.
21 S. Peigin, B. Epstein, T. Rubin and S. Séror. Parallel large scale high accuracy Navier-Stokes computations on distributed memory clusters, The Journal of Supercomputing, volume 27, number 1, pages 49–68, Springer, January 2004.
20 Boris Epstein, Theodor Rubin and Stéphane Séror. Accurate multiblock Navier-Stokes solver for complex aerodynamic configurations, AIAA journal, volume 41, number 4, pages 582–594, 2003.
19 S. Peigin, B. Epstein, T. Rubin and S. Séror. Parallel high accuracy CFD code for complete aircraft viscous flow simulations, in K. Matsuno, A. Ecer, N. Satofuka, J. Periaux and P. Fox (eds.), Parallel Computational Fluid Dynamics 2002, pages 507 – 514, North-Holland, 2003.
18 B. Epstein, S. Séror, S. Peigin and T. Rubin. Development of an accurate multiblock multiface parallel Navier-Stokes code NES with the Spallart-Almares model for complex aerodynamic configurations, in Aerospace Applications From High Subsonic to Hypersonic Regime, pages 460–469, 2002.
17 B. Epstein, I. Yavneh and A. Averbuch. An accurate ENO driven multigrid method applied to 3-D turbulent transonic flows, Journal of Computational Physics, volume 168, April 2001.
16 Amir Averbuch, Boris Epstein, Ludimila Ioffe and Irad Yavneh. Efficient parallelization of a three-dimensional Navier-Stokes solver on MIMD multiprocessors, The Journal of Supercomputing, volume 17, number 2, pages 123–142, Springer, January 2000.
15 B. Epstein, A. Jacobs and A. Nachshon. Aerodynamically accurate three-dimensional Navier-Stokes method, AIAA journal, volume 35, number 6, pages 1089–1090, 1997.
14 S. Peigin and B. Epstein. Massive Parallelization as Prinicipal Technology for Constrained Optimization of Aerodynamic Shapes, in G. Winter, A. Ecer, P. Fox, J. Periaux and N. Satofuka (eds.), Parallel Computational Fluid Dynamics 2004, pages 33—44, Elsevier Science, 1996.
13 Boris Epstein, Alexander L. Luntz and Aharon Nachshon. Cartesian Euler method for arbitrary aircraft configurations, AIAA journal, volume 30, number 3, pages 679–687, May 1992.
12 B. Epstein, A. L. Luntz and A. Nachshon. Multigrid transonic computations about arbitrary aircraft configurations, Journal of Aircraft, volume 26, number 8, pages 751–759, 1989.
11 A. Luntz and B. Epstein. A multigrid full potential transonic code for arbitrary configurations, GMD—Studien Nr 110 (German Institute for Mathematics and Data Processing), GMD Sankt-Augustin, pages 101–110, May 1986.
10 V. Rivkind and B. Epstein. The numerical method for solving non-stationary free boundary problems for the Navier-Stokes equations in curvilinear systems, Vestnik Leningrad Univ., volume 13, pages 79–83, 1984.
9 A. Luntz and B. Epstein. Modular potential flow computation including fuselage and wing tip effects, Israel Journal of Technology, volume 21, pages 76–80, 1983.
8 B. Epstein and V. Rivkind. Numerical experiment by projection schemes for the Navier-Stokes equations (Russian), Methods of Computation, (Metody Vichisl.), volume 10, pages 143-151, 1976.
7 V. Rivkind and B. Epstein. Alternating directions net schemes for solving the Navier-Stokes equations in orthogonal curvilinear coordinates, Transactions of the Seminar on Viscous Fluid Mechanics (Russian), Novosibirsk, volume 1, pages 90–95, 1976.
6 B. Epstein and V. Rivkind. Grid schemes with projection for the solution of the equations of the dynamics of viscous incompressible fluid (Russian, English summary), Vestnik Leningrad Univ., 13, Math. Mech. Astronom., volume 3, pages 144–147, 1975.
5 V. Rivkind and B. Epstein. Net schemes for the Navier- Stokes equations associated with projections, USSR Comp. Math. Physics, volume 15, pages 240–246, 1975.
4 B. Epstein. A scheme of variable directions type for the Navier-Stokes problem (Russian, English Summary), Vestnik Leningrad Univ., 7, Math. Mech. Astronom., volume 2, pages 166–168, 1974.
3 B. Epstein and V. Rivkind. Projection schemes for the solution of the Navier- Stokes equations in orthogonal curvilinear coordinates (Russian, English summary), Leningrad Univ., 13, Math. Mech. Astronom., volume 3, pages 56–63, 1974.
2 B. Epstein and V. Rivkind. High accuracy schemes for solving the Navier-Stokes equations (Russian), Numerical Methods in the Mechanics of Continuous Medium, volume 4, number 5, pages 105–111, 1973.
1 B. Epstein and A. Shuster. Construction of the tabular values in the numerical integration of a system of ordinary differential equations (Russian), Met. Vichisl., volume 8, pages 19–22, 1973.

Conference Proceedings

33 Boris Epstein and Sergey Peigin. Application of OPTIMENGA Software to Multi-point Multi-constrained Aerodynamic Design, in 54th AIAA Aerospace Sciences Meeting, 2016.
32 Boris Epstein and Sergey Peigin. Application of OPTIMENGA_AERO to Constrained Aerodynamic Design, in 53rd AIAA Aerospace Sciences Meeting, pages 1944, 2015.
31 Boris Epstein and Sergey Peigin. Aerodynamic Shape Optimization by Automatic Hybrid Genetic Tool OPTIMENGA_AERO, in 52nd Aerospace Sciences Meeting, pages 0569, 2014.
30 Boris Epstein and Sergey Peigin. 3D Optimization of Aerodynamic Wings Based on Accurate CFD Computations, in 43rd AIAA Aerospace Sciences Meeting and Exhibit, pages 454, 2012.
29 Sergey Peigin, Boris Epstein and Shlomit Gali. Design of Aerodynamic Shapes in Engineering Environment, in 44th AIAA Aerospace Sciences Meeting and Exhibit, pages 931, 2012.
28 Sergey Peigin and Boris Epstein. Incorporation of Fictitious Surfaces Into Aircraft Geometry for Aerodynamic Shape Optimization, in 46th AIAA Aerospace Sciences Meeting and Exhibit, pages 303, June 2012.
27 B. Epstein and S. Peigin. Parallel Treatment of non-matched grids for industrial Navier-Stokes simulations, in 22nd International Conference on Parallel Computational Fluid Dynamics, May 2010.
26 B. Epstein and S. Peigin. Treatment of non- matched grids for high- accuracy RANS solutions, in Proceedings of the 19th AIAA Computational Fluid Conference, AIAA paper, June 2009.
25 S. Peigin and B. Epstein. Efficient Parallel Algorithm for Aerodynamic Design of Wing-Body- Junction Driven by Accurate Navier-Stokes Computations, in 21st International Conference on Parallel Computational Fluid Dynamics, May 2009.
24 John Vassberg, Sergey Peigin, Antony Jameson, Boris Epstein, Dino Roman and Neal Harrison. A Pilot Project in Preparation of an Aerodynamic Optimization Workshop with Lessons Learned, in 26th AIAA Applied Aerodynamics Conference, pages 6226, 2008.
23 Sergey Peigin and Boris Epstein. CFD driven optimization of blended wing body aircraft, in 24th AIAA Applied Aerodynamics Conference, pages 3457, 2006.
22 Boris Epstein and Sergey Peigin. Robust Drag Minimization of Aerodynamic Shapes in Engineering Environment, in 23rd AIAA Applied Aerodynamics Conference, pages 5082, 2005.
21 Sergey Peigin and Boris Epstein. 3 D OPTIMIZATION OF AERODYNAMIC WINGS BASED ON ACCURATE CFD COMPUTATIONS, in 43 rd AIAA Aerospace Sciences Meeting and Exhibit, pages 2005, 2005.
20 Sergey Peigin and Boris Epstein. A Hybrid Approach to Multiconstraint Aerodynamic Optimization Driven by Full Navier-Stokes Computations, in 17th AIAA Computational Fluid Dynamics Conference, pages 4855, 2005.
19 B. Epstein and S. Peigin. Constrained optimization of aerodynamic shapes via minimization of total drag, in IPDO 2004 (Inverse Problems, Design and Optimizationymposium), Invalid Date.
18 Sergey Peigin, Boris Epstein, Teddy Rubin and Stefan Séror. Efficient Parallelization Strategy for a High Accuracy Navier-Stokes Algorithm, in 41st Aerospace Sciences Meeting and Exhibit, pages 430, 2003.
17 Stephane Séror, Theodor Rubin, Serguey Peigin and Boris Epstein. Implementation and Validation of the Spalart-Allmaras Turbulence Model for Parallel Processing on PC's Cluster, in 21st AIAA Applied Aerodynamics Conference, pages 3404, 2003.
16 S. Peigin and B. Epstein. Genetic Algorithms for optimization of aerodynamic shapes, in EUROGEN 2003 – Evolutionary Methods for Design, Optimization and Control, September 2003.
15 Boris Epstein and Sergey Peigin. A Robust Hybrid GA/ROM Approach to Multiobjective Constrained Optimization in Aerodynamics, in 16th AIAA Computational Fluid Dynamics Conference, pages 4092, August 2003.
14 B. Averbuch A. Braverman E. Epstein and Israeli M.. On substractional technique for fast direct spectral solution of Poisson and Helmholtz equations, in Proceedings of the 3rd International DCDIS Conference on Engineering Applications and Computational Algorithms, May 2003.
13 T. Arad E. Epstein B. Rubin and S. Seror. Recent enhancements of the 3D Navier- Stokes code NES, Proceedings of the 42nd Israel Conference on Aviation and Astronautics, 2002.
12 S. Epstein B Seror and T. Rubin. An accurate multiblock 3D ENO driven Navier-Stokes solver for complex aerodynamic configurations, in Proceedings of the 23rd International Congress of Aeronautical Sciences (ICAS 2002), September 2002.
11 T. Peigin S. Epstein B. Rubin and S. Seror. Parallel multiblock full Navier-Stokes code NES: 10 million points complete aircraft flow simulation, in Proceedings of the 42nd Israel Conference on Aviation and Astronautics, February 2002.
10 S. Seror, B. Epstein and T. Rubin. Construction of a multiblock 3-D full Navier- Stokes code for practical aerodynamic computations, in Proceedings of the 41st Israel Conference on Aviation and Astronautics, February 2001.
9 B. Epstein, A. Averbuch and I. Yavneh. An accurate ENO driven Multigrid method applied to 3-D turbulent transonic flows, in Proceedings of the 14th AIAA Computational Fluid Conference, pages 705–715, June 1999.
8 B. Epstein, A. Jacobs and A. Nachshon. Viscous computations by a 3-D ENO Navier-Stokes method, in Proceedings of the 37th Israel Conference on Aviation and Astronautics, pages 98-109, February 1997.
7 B. Epstein, A. Jacobs and A. Nachshon. An ENO 3-D multilevel Navier-Stokes method: towards an aerodynamically accurate CFD tool, in 15th International Conference on Numerical Methods in Fluid Mechanics, June 1996.
6 B Epstein and A Nachshon. An ENO Navier-Stokes solver applied to 2-D subsonic, transonic and hypersonic aerodynamic flows, in 32nd Aerospace Sciences Meeting and Exhibit, pages 303, 1994.
5 B. Epstein and A. Nachshon. An ENO 3-D Navier-Stokes solver applied to 2-D subsonic, transonic and hypersonic flows, in 32nd Aerospace Sciences Meeting, AIAA paper 94-0303, January 1994.
4 B. Epstein. New features in CFD technology at the TASHAN Engineering Center at IAI, in Proceedings of the 33rd Israel Conference on Aviation and Astronautics, pages 125–132, February 1993.
3 B. Epstein, A. Luntz and A. Nachshon. An Euler solver for arbitrary configurations: further applications, in Proceedings of the 31st Israel Conference on Aviation and Astronautics, pages 205–216, February 1990.
2 D. Aboudi, E. Baharav, B. Epstein, A. Luntz and M. Canard Shepshelovitch. LEF design for a multi-mission fighter aircraft, in Proceedings of 16th Congress of the International Council of the Aeronautical Sciences, ICAS, 88:3.11.1, pages 1700–1713, August 1988.
1 B. Epstein, A. Luntz and A. Nachshon. Multigrid computation of transonic flow about complex aircraft configurations, using Cartesian grids and local refinement, in Proceedings of 16th Congress of the International Council of the Aeronautical Sciences, ICAS, 88:4.7.3, pages 1038–1046, August 1988.
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