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Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants
Date
2018-07-11
Author
Özcan, Serhat
cürdaneli, sertaç
Ulaş, Abdullah
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This work is licensed under a
Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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URI
https://hdl.handle.net/11511/69353
DOI
https://doi.org/10.2514/6.2018-4578
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Department of Mechanical Engineering, Conference / Seminar
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S. Özcan, s. cürdaneli, and A. Ulaş, “Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants,” 2018, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/69353.