基于动力学模态分解法的绕水翼非定常空化流场演化分析$^{\bf 1)}$
谢庆墨*,陈亮†,张桂勇***,孙铁志***2)(
)
)
ANALYSIS OF UNSTEADY CAVITATION FLOW OVER HYDROFOIL BASED ON DYNAMIC MODE DECOMPOSITION$^{\bf 1)}$
Xie Qingmo*,Chen Liang†,Zhang Guiyong***,Sun Tiezhi***2)()
)
图8. $\sigma = 1.25$,$\sigma = 0.75$,$\sigma = 0.50$ 工况下模态 2 的对应流场流线图
Fig.8. Flow field streamline of mode 2 for $\sigma = 1.25$,$\sigma =0.75$,$\sigma = 0.50$
