Assertion: airfoil's lift | /r/HasProperty | computed with rng and sa turbulence models
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Source sentences:
text: Lift and drag coefficients, and , for the airfoil of 1 m chord are computed with RNG and SA turbulence models and compared at high Reynolds numbers (2.1 and 3.0 × 106) and at a lower Reynolds number (5.0 × 105).