| タイトル | An Assessment of CFD/CSD Prediction State-of-the-Art by Using the HART II International Workshop Data |
| 著者（英） | Biedron, Robert T.; Lim, Joon W.; Boyd, D. Douglas, Jr.; Min, Byung-Young; Smith, Marilyn J.; Baeder, James D.; Jung, Sung N.; Jayaraman, Buvana; vanderWall, Berend G. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2012-05-01 |
| 言語 | eng |
| 内容記述 | Over the past decade, there have been significant advancements in the accuracy of rotor aeroelastic simulations with the application of computational fluid dynamics methods coupled with computational structural dynamics codes (CFD/CSD). The HART II International Workshop database, which includes descent operating conditions with strong blade-vortex interactions (BVI), provides a unique opportunity to assess the ability of CFD/CSD to capture these physics. In addition to a baseline case with BVI, two additional cases with 3/rev higher harmonic blade root pitch control (HHC) are available for comparison. The collaboration during the workshop permits assessment of structured, unstructured, and hybrid overset CFD/CSD methods from across the globe on the dynamics, aerodynamics, and wake structure. Evaluation of the plethora of CFD/CSD methods indicate that the most important numerical variables associated with most accurately capturing BVI are a two-equation or detached eddy simulation (DES)-based turbulence model and a sufficiently small time step. An appropriate trade-off between grid fidelity and spatial accuracy schemes also appears to be pertinent for capturing BVI on the advancing rotor disk. Overall, the CFD/CSD methods generally fall within the same accuracy; cost-effective hybrid Navier-Stokes/Lagrangian wake methods provide accuracies within 50% the full CFD/CSD methods for most parameters of interest, except for those highly influenced by torsion. The importance of modeling the fuselage is observed, and other computational requirements are discussed. |
| NASA分類 | Aerodynamics |
| レポートNO | Paper No. 349
NF1676L-13580 |
| 権利 | Copyright |
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