@article{_n-s_2011,
	title = {{基于N}-{S方程的直升机旋翼翼型反设计方法}},
	issn = {1673-1220},
	abstract = {为了在实际旋翼翼型设计中考虑粘性影响,采用N-S方程为主控方程,建立了旋翼翼型流场求解方法。使用以Poisson方程为控制方程的网格生成程序生成围绕旋翼翼型的N-S粘性贴体网格,该网格生成程序能在反设计迭代过程中自动更新过渡翼型的粘性网格。在翼型流场计算及网格生成基础上,采用了MGM方程作为翼型反设计方程,建立了一套能够考虑粘性影响的直升机旋翼翼型的反设计方法。应用该方法,分别对二维NACA系列翼型、OA系列翼型、超临界翼型进行了反设计分析,获得了满足要求的二维旋翼翼型,并与目标值(压力分布、升力系数、阻力系数、力矩系数)吻合良好。},
	language = {中文;},
	number = {01},
	journal = {直升机技术},
	author = {万俊明;赵国庆;招启军;尚克明;},
	year = {2011},
	keywords = {MGM equation, MGM方程, N-S equations, N-S方程, airfoil, helicopter, inverse design, ⛔ No DOI found, 反设计, 直升机, 翼型},
	pages = {19--24},
}

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