Numeryczne wyznaczanie współczynników aerodynamicznych Cd, Cl i Cm w funkcji liczby Macha i kąta natarcia na przykładzie monolitycznego pocisku 5,56 × 45 mm NATO
- DOI
- 10.5281/zenodo.20090810
- Published
- 2025
- Container
- Not recorded
- Publisher
- Wydawnictwo Naukowe Kontekst, Kontekst Scientific Publisher
- Open access
- yes
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Cite this work
BibTeX
@article{allodium:10.5281/zenodo.20090810,
title = {Numeryczne wyznaczanie współczynników aerodynamicznych Cd, Cl i Cm w funkcji liczby Macha i kąta natarcia na przykładzie monolitycznego pocisku 5,56 × 45 mm NATO},
author = {Piłat, Kornel},
year = {2025},
doi = {10.5281/zenodo.20090810},
url = {https://doi.org/10.5281/zenodo.20090810}
}RIS
TY - JOUR TI - Numeryczne wyznaczanie współczynników aerodynamicznych Cd, Cl i Cm w funkcji liczby Macha i kąta natarcia na przykładzie monolitycznego pocisku 5,56 × 45 mm NATO AU - Piłat, Kornel PY - 2025 DO - 10.5281/zenodo.20090810 UR - https://doi.org/10.5281/zenodo.20090810 ER -
APA
Kornel, P. (2025). Numeryczne wyznaczanie współczynników aerodynamicznych Cd, Cl i Cm w funkcji liczby Macha i kąta natarcia na przykładzie monolitycznego pocisku 5,56 × 45 mm NATO. https://doi.org/10.5281/zenodo.20090810