Abstract
We consider a method of calculating the aerodynamic coefficients of bodies with arbitrary cross section. The method is carried out on electronic computers, and calculations for bodies with different aspect ratios and shapes are carried out by way of example. The effectiveness of the method is demonstrated by a comparison of the calculated results with the results of a systematic experiment.
Similar content being viewed by others
Literature cited
K. I. Babenko, G. P. Voskresenskii, A. N. Lyubimov, and V. V. Rusanov, Three-Dimensional Flow of an Ideal Gas past Smooth Bodies [in Russian], Nauka, Moscow (1964).
S. M. Gilinskii, G. F. Telenin, and G. P. Tinyakov, “Method of calculating supersonic flow past blunt bodies with a receding shock wave,” Izv. Akad. Nauk SSSR, Mekh. Mashinostr., No. 4 (1964).
Author information
Authors and Affiliations
Additional information
Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 6, pp. 92–98, November–December, 1977.
Rights and permissions
About this article
Cite this article
Skiba, G.G., Fedotov, B.N. Method of calculating aerodynamic coefficients of some three-dimensional bodies with arbitrary cross section. Fluid Dyn 12, 892–897 (1977). https://doi.org/10.1007/BF01090325
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF01090325