Hotspot


Acta Aeronautica et Astronautica Sinica | 2013

Study of Unsteady Separation Flow Around Airfoil at High Angle of Attack Using Hybrid RANS-LES Method

Liu Zhou; Yang Yunjun; Zhou Weijiang; Gong Anlong


Procedia Engineering | 2015

High-performance Computing of Periodic Unsteady Flow Based on Time Spectral Method☆

Xie Lijun; Yang Yunjun; Liu Zhou; Zhou Weijiang


Archive | 2017

A prediction method for aerodynamic characteristics of actual gaseous environment of Mars atmosphere

Zhan Huiling; Zhou Weijiang; Liu Zhou; Gong Anlong; Ji Chuqun


Yuhang Xuebao | 2016

数値シミュレーションにより,胴体の組合せ効果を研究した。【JST・京大機械翻訳】

Shi Lei; Liu Zhou; Yang Yunjun; Zhou Weijiang


Archive | 2016

Periodic unsteady flow field prediction method suitable for CFD numerical simulation

Xie Lijun; Yang Yunjun; Liu Zhou; Zhou Weijiang


Jixie Gongcheng Xuebao | 2016

台ガスタービン軸受の軸受動力学数値シミュレーションに関する研究【JST・京大機械翻訳】

Chen Guangqiang; Yang Yunjun; Lei Juanmian; Chen Bingyan; Liu Zhou


Procedia Engineering | 2015

Unstructured Adaptive Grid Refinement for Flow Feature Capture

Liu Zhou; Yang Yunjun; Gong Anlong; Zhou Weijiang


ACTA AERONAUTICAET ASTRONAUTICA SINICA | 2015

Unsteady numerical simulation of aerodynamic effect of a spinning projectile

Liu Zhou; Xie Lijun; Yang Yunjun; Zhou Weijiang


Archive | 2014

Method and device for rapidly calculating hypersonic viscosity force of aircraft

Gong Anlong; Ji Chuqun; Liu Zhou


ACTA AERONAUTICAET ASTRONAUTICA SINICA | 2014

A high efficient method for computing dynamic derivatives of aircraft based on time spectral method

Xie Lijun; Yang Yunjun; Liu Zhou; Zhou Weijiang

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