Özcan, S. Et Al. 2018. Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants. 2018 AIAA Propulsion and Energy Forum , (cincinnati, United States Of America).

Özcan, S., cürdaneli, s., & ULAŞ, A., (2018). Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants . 2018 AIAA Propulsion and Energy Forum, cincinnati, United States Of America

Özcan, Serhat, sertaç cürdaneli, And ABDULLAH ULAŞ. "Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants," 2018 AIAA Propulsion and Energy Forum, cincinnati, United States Of America, 2018

Özcan, Serhat Et Al. "Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants." 2018 AIAA Propulsion and Energy Forum , cincinnati, United States Of America, 2018

Özcan, S. cürdaneli, s. And ULAŞ, A. (2018) . "Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants." 2018 AIAA Propulsion and Energy Forum , cincinnati, United States Of America.

@conferencepaper{conferencepaper, author={Serhat Özcan Et Al. }, title={Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants}, congress name={2018 AIAA Propulsion and Energy Forum}, city={cincinnati}, country={United States Of America}, year={2018}}