Methods of assessing the aerodynamic characteristics of gliding munitions based on the results of their wreckage examination
DOI:
https://doi.org/10.34169/2414-0651.2024.4(44).52-57Keywords:
glide bomb, debris, aerodynamic characteristics, aerodynamic quality, weight and geometric parametersAbstract
The article presents the development of a methodology for the approximate operational assessment of the aerodynamic and flight-tactical characteristics of enemy aerial bombs using initial data obtained from the examination of debris from such munitions. The first stage of the methodology involves reconstructing the design solutions of such aviation weapons, determining their operational principles, as well as their weight and geometric parameters. The next stage calculates the main aerodynamic characteristics, and the final stage involves assessing the flight performance. The obtained data can subsequently be used in forming countermeasure proposals against such weapons and in substantiating technical solutions for the development of domestic analogs.
Downloads
References
Nykolaev , Y. M., Kushnir, S., Kaliuzhnyi , N. M., Silkov, V., Khriapkyn , A. V., Zirka, A., & Kravchuk, I. (2022). Improvement of bombardment with cabining as a way to increase the effectiveness of combat application of the aircraft for striking purposes. Weapons and Military Equipment, 31(3), 44–50. https://doi.org/10.34169/2414-0651.2021.3(31).44-50
Kravchuk, I.S. & Taranenko, V.V. (2019). Realizatsiia proportsiinoho samonavedennia korektovanoi aviatsiinoi bomby za informatsiieiu suputnykovoi systemy navihatsii. Nauka i tekhnika Povitrianykh Syl Zbroinykh Syl Ukrainy. № 3(36). Pp. 73—78.
Silkov , V., Zirka, A., & Arhipov , M. (2022). OPTIMIZATION OF COMBAT APPLICATION MODES AND DESIGN PARAMETERS OF AIR-TO-SURFACE CORRECTED WEAPONS. Weapons and Military Equipment, 34(2), 88–98. https://doi.org/10.34169/2414-0651.2022.2(34).88-98
Zirka, A. (2023). Methodology for estimating the values of the main parameters of bomb-throwing from cabrifi cation to ensure the implementation of the given bomb fl ight range based on the energy approach. Weapons and Military Equipment, 37(1), 40–44. https://doi.org/10.34169/2414-0651.2023.1(37).40-44
Bonch-Bruevych, H.F. (1977). Aerodynamycheskie kharakterystyky samoletov i ikh raschet. K.: KVVAYU. 95 p.
Bespylotni letatelni apparaty. Metodyky pryblyzhenykh raschetov osnovnykh parametriv i kharakterystyk. K.: TsNDY OVT. 2009. 301 p.
Rukovodstvo dlia konstruktorov letatelnykh apparatov samodeiatelnoi postroiky. Nsb.: 1994. 246 p.
Chumak, P.Y. & Kryvokrysenko, V.F. (1991). Raschet, proektirovanie i postroika sverkhlehkykh samoletov. M.: Patriot. 235 p.
Kotelnikov, H.N., Mamliuk, O.V., Silkov, V.I. & Tereshchenko, Yu.M. (2002). Aerodynamika litalnykh aparativ. K.: Vyshcha osvita. 255 p.
Downloads
Published
How to Cite
Issue
Section
License
Copyright (c) 2024 Валерій Сілков,Андрій Зірка
This work is licensed under a Creative Commons Attribution 4.0 International License.
