Cite
APA Citation
Armbruster, W., Hardi, J. S., Miene, Y., Suslov, D., & Oschwald, M. (2020). damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines. Acta astronautica, 169, 170–179. http://access.bl.uk/ark:/81055/vdc_100101586642.0x00004d