A Computer Software Application for the Design and Simulation of Unguided Rockets
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 t...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Military University of Technology, Warsaw
2020-06-01
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| Series: | Problemy Mechatroniki |
| Subjects: | |
| Online Access: | http://promechjournal.pl/gicid/01.3001.0014.1994 |
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| Summary: | 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. |
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| ISSN: | 2081-5891 |