Advances in simulation of wing and nacelle stall : results of the closing symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany
Advances in simulation of wing and nacelle stall : results of the closing symposium of the DFG Research Unit FOR 1066, December 1-2, 2014, Braunschweig, Germany
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DOI：
10.1007/978-3-319-21127-5
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发表时间：
2016
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影响因子：
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通讯作者：
R. Radespiel
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作者：
R. Radespiel
该书报告了模拟机翼和机舱失速问题的高级解决方案，国际公认的研究人员在DFG研究单位1066年度闭幕研讨会上提出并讨论了这一问题。在高雷诺数下对翼型、机翼和动力发动机舱的流动分离进行可靠的模拟，在定义合适的数学模型、计算精确的数值解和为数值模拟的验证提供全面的实验数据方面面临着巨大的挑战。其他问题产生于需要考虑机身-发动机相互作用和不均匀的起始流动条件，因为真实的飞机在具有往往很大扭曲的大气环境中运行。这本书详细报道了对这些问题和其他相关问题的基础和应用研究的结果，目标读者是所有对高级计算流体力学模型的开发感兴趣的读者、学者和专业人员，这些模型用于模拟具有流动分离的复杂飞机流动。
The book reports on advanced solutions to the problem of simulating wing and nacelle stall, as presented and discussed by internationally recognized researchers at the Closing Symposium of the DFG Research Unit FOR 1066. Reliable simulations of flow separation on airfoils, wings and powered engine nacelles at high Reynolds numbers represent great challenges in defining suitable mathematical models, computing numerically accurate solutions and providing comprehensive experimental data for the validation of numerical simulations. Additional problems arise from the need to consider airframe-engine interactions and inhomogeneous onset flow conditions, as real aircraft operate in atmospheric environments with often-large distortions. The findings of fundamental and applied research into these and other related issues are reported in detail in this book, which targets all readers, academics and professionals alike, interested in the development of advanced computational fluid dynamics modeling for the simulation of complex aircraft flows with flow separation.