Aplikacja komputerowa do projektowania i symulacji niekierowanych pocisków rakietowych
The paper presents a specification and performance characteristics of a computer software application developed for rocket design engineering. The methodology for the determination of aerodynamic characteristics by the software application is based on the Chernabrovkin-Lebyadyev’s experimental and theoretical method. The computer simulation results presented in the paper were generated for two types of 122-mm calibre rockets, M-21OF Grad and M-21FHE Feniks. The simulation results were verified with the results produced using other calculation methods.
Warszawa
oai:ribes-88.man.poznan.pl:2585
computer simulation, aerodynamic coefficients, rocket
Sep 30, 2025
Sep 30, 2025
0
https://ribes-88.man.poznan.pl/publication/2901
| Edition name | Date |
|---|---|
| A Computer Software Application for the Design and Simulation of Unguided Rockets | Sep 30, 2025 |
Krzysztof MOTYL Bogdan ZYGMUNT
Krzysztof MOTYL Mirosław MAKOWSKI, Bogdan ZYGMUNT, Zbigniew PUZEWICZ, Janusz NOGA
Krzysztof MOTYL Karol GĄSIOR
Krzysztof MOTYL Bogdan ZYGMUNT, Konrad SIENICKI,Janusz NOGA, Zbigniew PUZEWICZ