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Titlebook: Boundary Element Methods in Engineering; Proceedings of the I Balkrishna S. Annigeri,Kadin Tseng Conference proceedings 1990 Springer-Verla

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發(fā)表于 2025-3-21 18:58:41 | 只看該作者 |倒序?yàn)g覽 |閱讀模式
期刊全稱Boundary Element Methods in Engineering
期刊簡(jiǎn)稱Proceedings of the I
影響因子2023Balkrishna S. Annigeri,Kadin Tseng
視頻videohttp://file.papertrans.cn/191/190003/190003.mp4
圖書(shū)封面Titlebook: Boundary Element Methods in Engineering; Proceedings of the I Balkrishna S. Annigeri,Kadin Tseng Conference proceedings 1990 Springer-Verla
影響因子The Boundary Element Method (BEM) has become established as an effective tool for the solutions of problems in engineering science. The salient features of the BEM have been well documented in the open literature and therefore will not be elaborated here. The BEM research has progressed rapidly, especially in the past decade and continues to evolve worldwide. This Symposium was organized to provide an international forum for presentation of current research in BEM for linear and nonlinear problems in solid and fluid mechanics and related areas. To this end, papers on the following topics were included: rotary- wing aerodynamics, unsteady aerodynamics, design and optimization, elasticity, elasto- dynamics and elastoplasticity, fracture mechanics, acoustics, diffusion and wave motion, thermal analysis, mathematical aspects and boundary/finite element coupled methods. A special session was devoted to parallel/vector supercomputing with emphasis on mas- sive parallelism. This Symposium was sponsored by United Technologies Research Center (UTRC) , NASA Langley Research Center, and the International Association of Boundary Ele- ment Methods (lAB EM) . We thank the UTRC management for the
Pindex Conference proceedings 1990
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Time and Frequency Domain Aerodynamics for Flutter of Helicopter Rotors in Hovery-element formulation for unsteady potential incompressible flows is introduced. The results obtained for the aerodynamic forces, for pitch and flap, are compared with those typically used in the flutter analysis of rotors, (which are obtained using a strip-theory extension of Loewy’s formulation [3
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A General Purpose Fixed-Wing and Rotary-Wing Compressible Aerodynamics Analysis Method in which the wake and/or field influence is coupled into the linear Laplace solver through the boundary conditions. There are a number of advantages in using this approach. For instance, since the wake effect is “seen” as an induced velocity, any methodology that can provide this information may be
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Panel Methods for Multiple-Rotor Aerodynamicson. The earlier of the two is a full surface, time marching panel scheme based on Morino’s formulation. It has been implemented only for low speed (incompressible) flow. The second scheme uses an iterative coupling of the rotor velocity fields, decomposed into harmonics. Each field harmonic is compu
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A Vortex Method for Predicting Unsteady Flow and Boundary Layer Development Around an Airfoilminar and turbulent boundary layers are treated. By using even a rather small computer, reasonable prediction of starting flows around an airfoil of NACA23012 are obtained for various angles of attack either with or without boundary layer separation. The emphasis in the following article will be on
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A Unified Approach for Potential and Viscous Flows in Fixed-Wing and Rotary-Wing Aerodynamicsential aerodynamics and to introduce an extension of the formulation to compressible viscous flows. For the sake of simplicity, details of the formulation are given only for incompressible flows. For compressible flows, the formulations are only outlined. Also, because of space limitations no numeri
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