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强风干扰下固定翼无人机“元飞行”气动建模研究
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作者 章胜 刘刚 +2 位作者 周晓雨 黄江涛 朱喆 《宇航学报》 EI CAS CSCD 北大核心 2024年第8期1235-1250,共16页
强风干扰下的复杂空气动力学给固定翼无人机的安全稳定飞行带来了严峻挑战。为提高强风干扰下固定翼无人机的环境适应能力,发展了一种创新的“元飞行”气动建模方法。不同于传统气流系下的气动建模,“元飞行”气动建模是一种元方法论建... 强风干扰下的复杂空气动力学给固定翼无人机的安全稳定飞行带来了严峻挑战。为提高强风干扰下固定翼无人机的环境适应能力,发展了一种创新的“元飞行”气动建模方法。不同于传统气流系下的气动建模,“元飞行”气动建模是一种元方法论建模技术,其采用易于测量的飞行器相对于地面坐标系的运动变量进行描述,通过隔离实际飞行中难以观测到的风干扰影响,基于高阶泰勒展开多元函数变量分解理论,构建仅与无人机自身特性相关、不同风况条件下通用的固定翼无人机空气动力共性基函数解析模型,结合在线辨识的风干扰系数函数,进而实现对飞行器飞行过程中气动力(矩)的预测。研究表明文章发展的“元飞行”气动模型可以良好地预测未知风况下固定翼无人机的气动力(矩),为实时空气动力学建模的实现奠定了良好基础。 展开更多
关键词 固定翼无人机 气动建模 强风干扰 元飞行气动模型 空气动力共性基函数
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Parametric geometry representations for wind turbine blade shapes 被引量:3
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作者 Chen Jin Zhang Shiqiang +1 位作者 Hou Yi Eecen Peter 《High Technology Letters》 EI CAS 2011年第3期325-332,共8页
Based on the Joukowsky transformation and Theodorsen method, a novel parametric function (shape function) for wind turbine airfoils has been developed. The airfoil design space and shape control equations also have ... Based on the Joukowsky transformation and Theodorsen method, a novel parametric function (shape function) for wind turbine airfoils has been developed. The airfoil design space and shape control equations also have been studied. Results of the analysis of a typical wind turbine airfoil are shown to illustrate the evaluation process and to demonstrate the rate of convergence of the geometric characteristics. The coordinates and aerodynamic performance of approximate airfoils is rapidly close to the baseline airfoil corresponding to increasing orders of polynomial. Comparison of the RFOIL prediction and experimental results for the baseline airfoil generally show good agreement. A universal method for three-dimensional blade integration-" Shape function/Distribution function" is presented. By changing the parameters of shape function and distribution functions, a three dimensional blade can be designed and then transformed into the physical space in which the actual geometry is defined. Application of this method to a wind turbine blade is presented and the differences of power performance between the represented blade and original one are less than 0. 5%. This method is particularly simple and convenient for bodies of streamline forms. 展开更多
关键词 wind turbine AIRFOILS aerodynamic convergence shape function/ distribution function orders of polynomial (OP)
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Derivation of Varying Specific Heat Gasdynamic Functions,Normal Shock Analytical Solution and its Improvements 被引量:1
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作者 Tsui Chih-Ya Beijing University of Aeronautics and Astronautics,Beijing 100083,China 《Journal of Thermal Science》 SCIE EI CAS CSCD 1992年第4期235-240,共6页
A set of new gasdynamic functions with varying specific heat are derived for the first time.An original analytical solution of normal shock waves is worked out therewith.This solution is thereafter further improved by... A set of new gasdynamic functions with varying specific heat are derived for the first time.An original analytical solution of normal shock waves is worked out therewith.This solution is thereafter further improved by not involving total temperature.Illustrative examples of comparison are given,including also some approximate solutions to show the orders of their errors. 展开更多
关键词 varying specific heat gasdynamic function normal shock wave analytical solution improvement approximate solution
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An approach for shape optimization of stratosphere airships based on multidisciplinary design optimization 被引量:14
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作者 Ouan-bao WANG Ji-an CHEN Gong-yi FU Deng-ping DUAN 《Journal of Zhejiang University-Science A(Applied Physics & Engineering)》 SCIE EI CAS CSCD 2009年第11期1609-1616,共8页
Airship shape is crucial to the design of stratosphere airships. In this paper, multidisciplinary design optimization (MDO) technology is introduced into the design of airship shape. We devise a composite objective fu... Airship shape is crucial to the design of stratosphere airships. In this paper, multidisciplinary design optimization (MDO) technology is introduced into the design of airship shape. We devise a composite objective function, based on this technology, which takes account of various factors which influence airship performance, including aerodynamics, structures, energy and weight to determine the optimal airship shape. A shape generation algorithm is proposed and appropriate mathematical models are constructed. Simulation results show that the optimized shape gives an improvement in the value of the composite objective function compared with a reference shape. 展开更多
关键词 Airship shape Multidisciplinary design optimization (MDO) Adaptive simulation annealing Stratosphere airship
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