Laminarinio-turbulentinio virsmo vietos tyrimas FX 66-S-196 V1 sparno profilio paviršiuje
Abstract
Nagrinėjama virsmo vieta ant FX 66-S-196 V1 profilio, naudojant interaktyvią Marko Drelos (MIT) programą XFOIL. Gauti duomenys išanalizuoti ir palyginti su eksperimento rezultatais, gautais Delft technologijos universitete (Olandija) aerodinaminiame vamzdyje. Profilis buvo analizuojamas, kai Reinoldso skaičius buvo Re = 0,5·10.6 ir Re = 1,5·10.6. The transition location on the FX 66-S-196 V1 wing section was analyzed with the using interactive program XFOIL of Mark Drela, MIT. Calculated results of transition location were compared with published measurement data from a wind tunnel at Delft University of Technology (Netherlands). The airfoil was analyzed at the Reynolds number Re = 0,5·10.6 and Re = 1,5·10.6.