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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2008, Volume 49, Issue 3, Pages 109–113
(Mi pmtf1913)
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This article is cited in 5 scientific papers (total in 5 papers)
Calculation of pressure on an airfoil contour in an unsteady separated flow
D. N. Gorelov Omsk Department of the Sobolev Institute of Mathematics, Siberian Division, Russian Academy of Sciences, Omsk, 644099
Abstract:
Simple formulas for calculating the pressure and the total hydrodynamic reactions acting on an arbitrarily moving airfoil are derived within the framework of the model of plane unsteady motion of an ideal incompressible fluid. Several vortex wakes may be shed from the airfoil owing to changes in velocity circulation around the airfoil contour. Cases with nonclosed and closed contours are considered.
Keywords:
separated flow around an airfoil contour, unsteady flow, pressure calculation.
Received: 27.02.2007 Accepted: 22.06.2007
Citation:
D. N. Gorelov, “Calculation of pressure on an airfoil contour in an unsteady separated flow”, Prikl. Mekh. Tekh. Fiz., 49:3 (2008), 109–113; J. Appl. Mech. Tech. Phys., 49:3 (2008), 437–441
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https://www.mathnet.ru/eng/pmtf1913 https://www.mathnet.ru/eng/pmtf/v49/i3/p109
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Abstract page: | 30 | Full-text PDF : | 8 |
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