SPLINE-FUNCTIONS IN THE TASK OF THE FLOW AIRFOIL PROFILE
DOI:
https://doi.org/10.18372/2306-1472.57.5536Keywords:
airfoil profile, spline-function, the potential flow, velocity at the profile contourAbstract
The method and the algorithm of solving the problem of streamlining are presented. Neumann boundary problem is reduced to the solution of integral equations with given boundary conditions using the cubic spline-functionsReferences
Lopatjuk, M.M. 2011. Spline - functions in hydroaeromechanics problems. Kyiv, Water Transport. KDAVT scientific papers collection. N 2 (15): 147150 (in Ukrainian).
Lopatjuk, M.M. 2011. The mathematics model of the limited span wing using the spline-functions. Materials X International Scientific and Technical Conference “AVIA-2011”. Kyiv, National Aviation University. Vol. 1: 6.346.37 (in Ukrainian).
Pavlovets, G.A. 1971. Methods of calculation of wing sections streamlining of perfect incompressible flow. Moscow, Proceedings of the TsAGI. Vol. 1344 (in Russian).
Zavialov, J.S.; Kvasov, B.I.; Miroshnichenko, V.L. 1980. Methods of spline - functions. Moscow, Nauka. 352 p. (in Russian).
Lopatjuk, M.M. 2011. The mathematics model of the limited span wing using the spline-functions. Materials X International Scientific and Technical Conference “AVIA-2011”. Kyiv, National Aviation University. Vol. 1: 6.346.37 (in Ukrainian).
Pavlovets, G.A. 1971. Methods of calculation of wing sections streamlining of perfect incompressible flow. Moscow, Proceedings of the TsAGI. Vol. 1344 (in Russian).
Zavialov, J.S.; Kvasov, B.I.; Miroshnichenko, V.L. 1980. Methods of spline - functions. Moscow, Nauka. 352 p. (in Russian).
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Published
21-01-2014
How to Cite
Lopatjuk, M. (2014). SPLINE-FUNCTIONS IN THE TASK OF THE FLOW AIRFOIL PROFILE. Proceedings of National Aviation University, 57(4), 53–55. https://doi.org/10.18372/2306-1472.57.5536
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MODERN AVIATION AND SPACE TEHNOLOGY