Axial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validation
- DOI
- 10.3390/polym13040517
- Published
- 2021-02-09
- Container
- Polymers
- Publisher
- MDPI AG
- Open access
- unknown
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Cite this work
BibTeX
@article{allodium:10.3390/polym13040517,
title = {Axial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validation},
author = {Rajesh Mishra and Bijoy Kumar Behera and Sayan Mukherjee and Michal Petru and Miroslav Muller},
year = {2021},
journal = {Polymers},
doi = {10.3390/polym13040517},
url = {https://doi.org/10.3390/polym13040517}
}RIS
TY - JOUR TI - Axial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validation AU - Rajesh Mishra AU - Bijoy Kumar Behera AU - Sayan Mukherjee AU - Michal Petru AU - Miroslav Muller PY - 2021 JO - Polymers DO - 10.3390/polym13040517 UR - https://doi.org/10.3390/polym13040517 ER -
APA
Mishra, R., Behera, B. K., Mukherjee, S., Petru, M., & Muller, M. (2021). Axial and Radial Compression Behavior of Composite Rocket Launcher Developed by Robotized Filament Winding: Simulation and Experimental Validation. Polymers. https://doi.org/10.3390/polym13040517
Source records
- crossref · retrieved 2026-09-26T02:50:36.404Z