首页> 外文会议>ASME turbo expo conference >UNSTEADY AERODYNAMIC FORCES ON VIBRATING ANNULAR CASCADE BLADES - CROSS-VALIDATION OF THE LINEAR UNSTEADY CFD CALCULATIONS USING THE TVD SCHEME AND THE DOUBLE LINEARIZATION THEORY -
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UNSTEADY AERODYNAMIC FORCES ON VIBRATING ANNULAR CASCADE BLADES - CROSS-VALIDATION OF THE LINEAR UNSTEADY CFD CALCULATIONS USING THE TVD SCHEME AND THE DOUBLE LINEARIZATION THEORY -

机译:在振动环形级联刀片上的不稳定空气动力 - 使用TVD方案的线性非稳态CFD计算的交叉验证及双线性化理论 -

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The paper presents the formulation to compute numerically the unsteady aerodynamic forces on the vibrating annular cascade blades. The formulation is based on the finite volume method, the type, and the TVD scheme, following the UPACS code developed by NAL, Japan. By applying the TVD scheme to the linear unsteady calculations, the precise calculation of the peak of unsteady aerodynamic forces at the shock wave location like the delta function singularity becomes possible without empirical constants. As a further feature of the present paper, results of the present numerical calculation are compared with those of the double linearization theory (DLT), which assumes small unsteady and steady disturbances but the unsteady disturbances are much smaller than the steady disturbances. Since DLT requires far less computational resources than the present numerical calculation, the validation of DLT is quite important from the engineering point of view. Under the conditions of small steady disturbances, a good agreement between these two results is observed, so that the two codes are cross-validated. The comparison also reveals the limitation on the applicability of DLT.
机译:本文呈现了在振动环形级联叶片上计算数值不稳定的空气动力学的配方。根据NAL,日本NAL开发的UPACS代码,该配方基于有限体积法,类型和TVD方案。通过将TVD方案应用于线性不稳定的计算,可以在没有经验常量的情况下,如Delta函数奇点的冲击波位置处的非定常空气动力力的峰的精确计算成为可能。作为本文的另一个特征,将本数值计算的结果与双线性化理论(DLT)进行比较,这假设小的不稳定和稳定的扰动,但不稳定的干扰远小于稳定的干扰。由于DLT需要较少的计算资源而不是本数值,因此DLT的验证是从工程的角度来看非常重要。在小稳定干扰的条件下,观察到这两个结果之间的良好一致性,因此两种代码是交叉验证的。比较还揭示了DLT适用性的限制。

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