YUAN Xiang-jiang, TU Guo-hua, ZHANG Han-xin, Shen Qing. Disturbance waves evolvement influenced by shock-boundary interaction[J]. ACTA AERODYNAMICA SINICA, 2006, 24(1): 22-27.
Citation: YUAN Xiang-jiang, TU Guo-hua, ZHANG Han-xin, Shen Qing. Disturbance waves evolvement influenced by shock-boundary interaction[J]. ACTA AERODYNAMICA SINICA, 2006, 24(1): 22-27.

Disturbance waves evolvement influenced by shock-boundary interaction

More Information
  • Available Online: January 07, 2021
  • Related Articles

    [1]FENG Shuo, WANG Bofu, TU Guohua, WU Jianhui, CHEN Jianqiang, YANG Qiang. Influence of cavities on hypersonic boundary layer transition[J]. ACTA AERODYNAMICA SINICA, 2023, 41(11): 56-70. DOI: 10.7638/kqdlxxb-2022.0169
    [2]FAN Xiaohua, ZHANG Qinghu, LUO Lei, LIN Jingzhou, TANG Zhigong. Flow-field characteristics analyses on shock-wave/boundary-layer interaction of TSTO parallel separation[J]. ACTA AERODYNAMICA SINICA, 2023, 41(5): 87-97. DOI: 10.7638/kqdlxxb-2022.0184
    [3]WANG Dexin, CHU Youbiao, LIU Nansheng, LI Zhufei, YANG Jiming. Numerical investigation of shock wave/boundary layer interactions near a convex corner[J]. ACTA AERODYNAMICA SINICA, 2020, 38(1): 148-159. DOI: 10.7638/kqdlxxb-2019.0111
    [4]YAO Yao, GAO Bo. Flow structure of incident shock wave boundary layer interaction with separation[J]. ACTA AERODYNAMICA SINICA, 2019, 37(5): 740-747, 769. DOI: 10.7638/kqdlxxb-2018.0155
    [5]Gao Zhi. Interacting shear flow stability theory with application to improving computational method of simulating numerically high Reynolds number flows[J]. ACTA AERODYNAMICA SINICA, 2015, 33(2): 183-191. DOI: 10.7638/kqdlxxb-2014.0098
    [6]ZHAO Yunfei, LIU Wei, LIU Xu, DENG Xiaogang. Unsteady shock/boundary layer interaction of compression corner at movement conditions[J]. ACTA AERODYNAMICA SINICA, 2014, 32(5): 610-617. DOI: 10.7638/kqdlxxb-2014.0089
    [7]YE Xing-fu, FANG Yi-hong. A numerical study for the generation of shocklet by 3-D disturbances in supersonic boundary layer[J]. ACTA AERODYNAMICA SINICA, 2007, 25(3): 281-286.
    [8]Favorable influence of swept shock-boundary layer interactions[J]. ACTA AERODYNAMICA SINICA, 2004, 22(2): 220-224.
    [9]SHEN Yi-qing, GAO Zhi, WANG Ru-quan. DPNS Scheme and NS Scheme Computing Shock-wave/Boundary Layer Interaction Flow With Secondary Vortices[J]. ACTA AERODYNAMICA SINICA, 2000, 18(4): 407-412.
    [10]Mao Xiaohai, Lu Xiyun, Zhuang Lixian. Numerical Study on the Interaction between a Shock Wave and a Compressible Vortex Ring[J]. ACTA AERODYNAMICA SINICA, 1999, 17(2): 203-211.

Catalog

    Article views (1645) PDF downloads (1208) Cited by()

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return