Combustion Performance Comparison of Propellant Grain for Hybrid Rocket Motors Manufactured by Casting and Fused Deposition Modeling
Author:
Publisher
EJournal Publishing
Subject
Artificial Intelligence,Mechanical Engineering,Control and Systems Engineering
Link
http://www.ijmerr.com/uploadfile/2019/0923/20190923042319501.pdf
Cited by 14 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
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2. Transient numerical investigation on thermochemical erosion of C/C nozzles in hybrid rocket motors;Journal of Physics: Conference Series;2024-05-01
3. Numerical Analysis on Nozzle Erosion in Hybrid Rocket Motors with Different Injection Parameters;2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE);2023-07-18
4. Dynamic Numerical Simulation of Hybrid Rocket Motors with Fuel Containing Aluminum Hydride;2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE);2023-07-18
5. Numerical Analysis of Hybrid Rocket Motor with Star-Wheel Segmented Grain;2023 14th International Conference on Mechanical and Aerospace Engineering (ICMAE);2023-07-18
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