Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants

2018-07-11
Özcan, Serhat
cürdaneli, sertaç
Ulaş, Abdullah
Citation Formats
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.