期刊文献+

旋成体零攻角纵向大扰动势流的AF-2迭代及其并行算法

AF 2 ITERATION AND ITS PARALLEL ALGORITHM FOR TRANSONIC FLOW WITH LARGE DISTURBANCES IN FREESTREAM-DIRECTION AROUND AXISYMMETRIC BODIES AT ZERO ANGLE OF ATTACK
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摘要 1.引言 为提高跨音速差分计算效率,人们在计算格式的设计、改进方面做了大量的工作,并取得了可喜的成就。并行计算机的出现和发展,使我们有可能进一步提高计算效率。第9期阂赛金等:旋成体零攻角纵向大扰动势流的人F一2迭代及其并行算法A弓n因为并行处理机具有处理数据能力强、计算效益高的特点,但这种机器必须结合具体问题和机器特点加以考虑才能发挥其优势。目前,利用我国设计的“YH一1”(“银河一1”)亿次并行处理机。 The calculations of AF-2 scheme are made by serial algorithm and parallel algorithm on computer''Yinhe-l'for solving axisymme-trical transonic potential equation with large disturbances in the freestream direction and small disturbance in the radial direction. By computations, the convergence of AF-2 is compared with that of SLOR, and the efficiency for parallel algorithm of AF-2 is compared with the efficiency for serial algorithm. Results indicate rhat A.F-2 technique has led to a 3-7 fold improvement in convergence against SLOR. and the computation efficiency by the parallel algorithm of AF-2 is about 3 times higher than that by the serial algorithm of AF-2.
出处 《航空学报》 EI CAS CSCD 北大核心 1990年第9期A510-A514,共5页 Acta Aeronautica et Astronautica Sinica
关键词 轴对称体 跨音速流 势流 零攻角 axisymmetrie bodies, transonic flow, potential flow,numerical caculation.
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参考文献3

  • 1李秀英,1986年
  • 2罗时钧,1983年
  • 3罗时钧,跨音速定常势流的混合差分法,1979年

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