Investigation of aerodynamic characteristics of NACA0012 airfoil design using parabolic arcs

Author:

Devi Supriya,Nagaraja K.V.

Publisher

Elsevier BV

Subject

General Medicine

Reference18 articles.

1. Theory of wing sections: including a summary of airfoil data;Abbott;Courier Corporation.,2012

2. R.H. Oppermann, 1938. National advisory committee for aeronautics: Report No. 624, Two-Dimensional Subsonic Compressible Flow Past Elliptic Cylinders, by Carl Kaplan. 8 pages, illustrations, 23× 29 cms. Washington, Government Printing Office, 1938. Price 10 cents.

3. E.N. Jacobs, 1932. The aerodynamic characteristics of eight very thick airfoils from tests in the variable density wind tunnel.

4. F.W. Schmitz, 967. Aerodynamics of the model airplane. Part 1. Airfoil measurements. Translated from German by Translation Branch, Redstone Scientific Information Center.Research and Development Directorate, United States Army Missile Command, Redstone Arsenal, Al-abama,35809.

5. K.K. Gupta, J.L. Meek, 2003. Finite element multidisciplinary analysis. American Institute of aeronautics and astronautics.

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Pressure and flow transition over NACA airfoil with thrust optimized parabolic arcs;International Journal of Modern Physics B;2023-07-25

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