Journal of aircraft, 2005-09, Vol.42 (5), p.1362-1366
2005
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Details
- Autor(en) / Beteiligte
- Titel
- Automatic Transition Prediction for High-Lift Systems Using a Hybrid Flow Solver
- Ist Teil von
- Journal of aircraft, 2005-09, Vol.42 (5), p.1362-1366
- Ort / Verlag
- Reston, VA: American Institute of Aeronautics and Astronautics
- Erscheinungsjahr
- 2005
- Quelle
- Alma/SFX Local Collection
- Beschreibungen/Notizen
- The first application of a coupled system consisting of a hybrid TAU code and the transition prediction module to a high-lift multi-element configuration is presented. Using a laminar boundary-layer method between the Reynolds averaged Navier-Stokes (RANS) solver and the eN-database method shows high potential over the use of boundary-layer parameters computed directly from the RANS grid.
- Sprache
- Englisch
- Identifikatoren
- ISSN: 0021-8669eISSN: 1533-3868DOI: 10.2514/1.16173Titel-ID: cdi_crossref_primary_10_2514_1_16173
- Format
- –
- Schlagworte
- Aerodynamics, Aircraft, Applied fluid mechanics, Boundary layer, Computational methods in fluid dynamics, Exact sciences and technology, Fluid dynamics, Fundamental areas of phenomenology (including applications), Physics, Predictive control, Transition to turbulence, Turbulent flows, convection, and heat transfer