Prediction of hysteresis associated with static stall of an airfoil
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چکیده
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An Experimental Study of Stall Hysteresis of a Low-Reynolds-Number Airfoil
An experimental study was conducted to investigate static stall hysteresis of a NASA GA(W)-1 airfoil at the chord Reynolds number of Re = 162,000. In addition to mapping the surface pressure distribution around the airfoil, a digital PIV system was used to make detailed flowfield measurements to quantify the occurrence and behavior of laminar boundary layer separation and transition on the airf...
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Aerodynamic Hysteresis of a Low- Reynolds-Number Airfoil
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ژورنال
عنوان ژورنال: AIAA Journal
سال: 2000
ISSN: 0001-1452,1533-385X
DOI: 10.2514/3.14499