NACA0012, NACA4412, RAE2822 airfoil and ONERA M6 wing, delta wing, slender body of missile and TND-712 wing-body standard model were chosen to confirm the validity of the current multigrid method.

 
  • 選用了NACA0012翼型、NACA4412翼型、RAE2822翼型、ONERA M6機翼、大后掠三角翼、細長(cháng)旋成導彈體及TND-712翼身組合體等多個(gè)算例對本文使用的多重網(wǎng)格方法進(jìn)行了驗證。
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