Cite
HARVARD Citation
Armbruster, W. et al. (2020). Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines. Acta astronautica. pp. 170-179. [Online].
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Armbruster, W. et al. (2020). Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines. Acta astronautica. pp. 170-179. [Online].