المؤلفون: Shen Xin, Zhang Liang, Dong Meng, Chen Jing

المصدر: Hangkong bingqi, Vol 30, Iss 5, Pp 86-91 (2023)

مصطلحات موضوعية: composite solid propellant, “dewetting” point, strain rate, mesoscale model, numerical simulation, Motor vehicles. Aeronautics. Astronautics, TL1-4050

وصف الملف: electronic resource

Relation: https://www.aeroweaponry.avic.com/fileup/1673-5048/PDF/2023-00073.pdf; https://doaj.org/toc/1673-5048

URL الوصول: https://doaj.org/article/439f3537e99a45669c54990f45518ff2