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气动与隐身性能计算精度对飞行器设计的影响 被引量:8

Influence of Aerodynamic and Stealth Performance Computation Precision on Aircraft Optimization Design
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摘要 将计算精度高的流场和电磁场求解算法引入到飞行器外形多目标优化设计中,研究了气动特性和雷达散射截面算法计算精度对外形设计结果的影响。以无人机外形气动与隐身一体化设计为例的研究结果表明,低精度优化设计的外形在实际应用中难以获得预期的性能,采用高精度计算模型的优化设计可以获得性能更优的外形。 The high-precision algorithms about CFD and electromagnetism are inducted in the aircraft configuration multi-objective optimization design. For the aerodynamic performance and the radar cross section, the influence of the computational method models precision on aircraft configuration optimization design is researched. An unmanned air vehicle configuration is designed to improve the aerodynamic performance and the stealth performance as an example. The results show, the configuration designed by using the low-precision algorithms can not acquire the anticipative performance in fact, and the configuration designed by using high-precision algorithms is of better performance than the low-precision optimization configuration.
出处 《飞行力学》 CSCD 北大核心 2009年第6期14-17,共4页 Flight Dynamics
基金 国家自然科学基金资助项目(90205020)
关键词 雷达散射截面 多目标优化 无人机 radar cross section multi-objective optimization unmanned air vehicle
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  • 1胡俊,聂在平,雷霖,王军.三维局部多层快速多极子算法[J].系统工程与电子技术,2006,28(3):329-330. 被引量:5
  • 2SOBIECZKY H. Parametric airfoils and wings[J]. Note on Numerical Fluid Mechanics. 1998. 71-88. Vieweg.
  • 3LIOU M S. Progress towards an improved CFD method: AUSM+ [R].AIAA95-1701.
  • 4BALDWIN B S, LOMAX H. Thin layer approximation algebraic model for separated turbulent flow[R]. AIAA78-257, 1978.
  • 5POWELL M J D. An efficient method for finding the minimum of a function of several variables without calculation derivatives[J]. Computer Journal, 1964, 7(2): 155-162.
  • 6HICKS R M, HENNE P A. Wing design by numerical optimization[R]. AIAA 77-1247.
  • 7阮颖铮.雷达截面与隐身技术[M].北京:国防工业出版社,1998..
  • 8CROSSLEY W A,et al.Using the two-branch tournament genetic algorithm for multiobjective design[R].AIAA-98-1914,1998.
  • 9MASKEW B.Prediction of subsonic aerodynamic characteristics:a case for low-order panel methods[J].Journal of Aircraft.1992,19(2):157-163.
  • 10KIM Y,YEE K,LEE D H.Aerodynamic shape design of rotor airfoils undergoing unsteady motion[ J].Journal of Aircraft.2004,41(2):247-257.

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