Computation of delta wing flap oscillations with a Reynolds-averaged Navier-Stokes solver

Alexander Allen, Michail Iatrou, Alexander Pechloff, Boris Laschka

Research output: Contribution to journalArticlepeer-review

2 Scopus citations

Abstract

A selection of steady and unsteady validation results for the Reynolds-averaged Navier-Stokes solver FLM-NS with respect to an experimental delta wing test case is presented and compared to other numerical results. Having put the numerical method's validity into evidence, the unsteady flow induced by an oscillating flap is investigated for a Fighter Type Delta Wing.

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