Constructing the External Contour of the Frankl Nozzle Using S-Shaped Curves with Quadratic Distribution of the Curvature

Author:

Stetsyuk P. I.,Tkachenko O. V.,Khomyak O. M.,Gritsay O. L.

Publisher

Springer Science and Business Media LLC

Subject

General Computer Science

Reference22 articles.

1. V. E. Alemasov, A. F. Dregalin, and A. P. Tishin, Theory of Rocket Engines [in Russian], Mashinostroyeniye, Moscow (1984).

2. D. A. Melnikov, U. G. Pirumov, and A. A. Sergienko, “Nozzles of jet engines,” in: Aeromechanics and Gas Dynamics [in Russian], Nauka, Moscow (1976), pp. 57–75.

3. F. I. Frankl, “To the theory of the Laval nozzles,” Izv. Akad. Nauk SSSR, Ser. Mat., Vol. 9, No. 5, 387–422 (1945).

4. A. A. Sergienko, V. V. Semenov, and A. A. Sobachkin, Selection of the Optimal Size and Contour of the Circular Nozzle [in Russian], MAI, Moscow (2004).

5. V. Mikhailenko and S. Ustenko, “The role of applied geometry to improve the efficiency of turbomachines,” Heometrychne Modelyuvannya ta Informatsiyni Tekhnolohiyi, No. 1, 82–86 (2016).

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