Calculation of transonic flows around profiles with blunt and angled leading edges
نویسندگان
چکیده
منابع مشابه
ThePressure-Drag due to Blunt Leading Edges on Two-Dimensional Aerofoils, at Transonic and Low-Supersonic Speeds
Pressure drags, obtained from measured pressure distributions in the transonic and low-supersonic speed range, are compared for sharp and blunt leading-edged two-dimensional aerofoils. For the special blunt shapes considered here, the high pressures in the stagnation-point region are offset by low pressures generated further round on the leading edge and on the basic aerofoil itself. The result...
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ژورنال
عنوان ژورنال: Vietnam Journal of Mechanics
سال: 2016
ISSN: 0866-7136,0866-7136
DOI: 10.15625/0866-7136/38/1/4177