Düz Uçuş için Kanat Profili Eniyilemesi

Author:

Körpe Sinan,Darak Hakan

Publisher

Journal of Aviation

Subject

General Earth and Planetary Sciences,General Environmental Science

Reference1 articles.

1. [1] Zang, T.A. (2010) "Airfoil/Wing Optimization." Encyclopedia of Aerospace Engineering. Online Publication DOI: 10.1002/9780470686652.eae500 [2] Garcia, M.J. , Boulanger, P. , Giraldo, S. “CFD Based Wing Shape Optimization Through Gradient-Based Method” EngOpt 2008 - International Conference on Engineering Optimization Rio de Janeiro, Brazil, 01 - 05 June 2008 [3] NACA 4 Hane hesaplama yöntemi, Erişim tarihi: 29.12.2016 http://airfoiltools.com/airfoil/naca4digit [4] Everstine, G.C. (2010) Numerical Solution of Partial Differential Equations Erişim Tarihi: 05.01.2016 http://gwu.geverstine.com/pdenum.pdf [5] Körpe, S.D. ve Özgen S (2016) “Morphing Wing Optimization for Steady Level Flight” Proc IMechE Part G: J Aerospace Engineering DOI: 10.1177/0954410016662063 [6] Darak, H “Düz Uçuş için Kanat Profili Eniyilemesi” Yüksek lisans tezi, Türk Hava Kurumu Üniversitesi, 2017. [7] Edelman, L. XFoil-MATLAB ortak arayüzü Erişim Tarihi: 10.11.2016 https://www.mathworks.com/matlabcentral/fileexchange/49706-xfoil-interface-updated

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