Equations of state for thrust modeling of ram accelerator at different bores
(2017)
Presentation / Conference
Bauer, P., Bengherbia, T., Yao, Y., Knowlen, C., Bruckner, A., & Giraud, M. (2017, September). Equations of state for thrust modeling of ram accelerator at different bores. Presented at Italian Association of Aeronautics and Astronautics XXIV International Conference, Palermo – Enna, Italy
The ram accelerator is a propulsion concept based on using shock-induced combustion to accelerate projectiles traveling at supersonic speeds in a launch tube pre-filled with a gaseous combustible mixture. Extensive experimental studies have been carr... Read More about Equations of state for thrust modeling of ram accelerator at different bores.