Partitioned subiterative coupling schemes for aeroelasticity using combined interface boundary condition method

Publisher: Taylor & Francis Ltd

E-ISSN: 1029-0257|28|6-10|272-300

ISSN: 1061-8562

Source: International Journal of Computational Fluid Dynamics, Vol.28, Iss.6-10, 2014-07, pp. : 272-300

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Abstract