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用于旋翼飞机开发研究的多分野解析框架OA北大核心CSTPCD

Multidisciplinary Analysis Framework for Rotorcraft Research and Development

中文摘要英文摘要

介绍了日本宇宙航空研究开发机构研发的用于旋翼飞机的多分野解析框架.HeliDesign是在各种旋翼飞机初期概念设计时使用的软件;rFlight可以提供在各种飞行条件下的平衡解析和线性化飞行模型;rBET/RMT是基于叶片要素理论的低保真度空力解析软件,和rMode提供的结构模型结合,可以推测旋转翼的弹性变形和各种飞行条件下的空力负载;rFlow3D是基于CFD计算的高保真度数值模拟软件;rGrid系列自动网格构造工具为其提供简单的网格生成;基于rFlow3D的计算结果,rNoise可以预测在任何观测点的噪声.这些软件已经广泛地被应用在各种新型旋翼飞机的开发研究中,其计算精度也已被各种实验结果所应证.

A multidisciplinary analysis toolchain specifically for rotorcraft has been developed at JAXA.HeliDesign provides the sizing of a conventional or a compound helicopter to meet the specified mission requirement based on preliminary semi-empirical relations.rFlight delivers the trim analysis and performance of a rotorcraft together with the linearized flight dynamics models based on analytical formulations of the rotor aerodynamics from blade-element theory.rBET/RMT is a low fidelity tool based on blade-element theory.For high-fidelity aeroelastic analysis of a rotating blade,rFlow3D is constructed based on high-resolution CFD and loosely coupled with computational structural dynamics(CSD)to obtain the elastic deformations of a rotor blade,while the natural frequencies and modes are obtained using rMode.rGrid tools support the automatic grid generations around a rotor blade to be computed in rFlow3D.Acoustic signature from a rotorcraft can be predicted using rNoise based on the FW-H equations using the output from rFlow3D.These tools have been applied for new rotorcraft developments and the high-fidelity toolchain has been validated with reliable test data with satisfactory accuracy.

TANABE Yasutada;SUGAWARA Hideaki;KIMURA Keita

日本宇宙航空研究开发机构航空技术部,东京181-0015,日本

旋翼飞机多分野解析高保真模拟设计工具

rotorcraftmultidisciplinary analysishigh-fidelity simulationsdesign tools

《南京航空航天大学学报(英文版)》 2024 (001)

43-52 / 10

10.16356/j.1005-1120.2024.01.003

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