AOTV bluff body flow - Relaxation algorithm

Author:

LOMBARD C.1,BARDINA J.1,VENKATAPATHY E.1

Affiliation:

1. PEDA Corp., Palo Alto, CA

Publisher

American Institute of Aeronautics and Astronautics

Reference34 articles.

1. This scheme would appear to have two virtues. The first is, linearl, the truncation error 0(h2), reduced hg a factor of 4 over either difference operator alone. The second is that the terms with one-quarter weights on either side of the firstorder upwind contributions (with weight one) are balanced. Since both sets of these terms with one-quarter weight are of themselves destabilizing, through the contribution of a wrong eigenvalue sign, balancing them with minimum weight for either can, on the a\rerage, be expected to minimize their adverse impact on robustness in the real case of variable coefficients. For this second-order scheme, the first-order upwind contributions to the diagonal are highly stabilizing in the sense of 'eonard.2s -4xisymmetric Flow Results

2. This work was partially supported by NASA Ames Research Center under Contract NAS2-11920, by AFOSR under Contract F4962G83-C-0084 and by ARO under Contract D-L4G29-84C-0002.

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Upwind-biased, point-implicit relaxation strategies for viscous, hypersonic flows;9th Computational Fluid Dynamics Conference;1989-06-13

2. Blunt-body flow simulations;24th Joint Propulsion Conference;1988-07-11

3. Application of program LAURA to three-dimensional AOTV flowfields;24th Aerospace Sciences Meeting;1986-01-06

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