Results 131 to 140 of about 11,282 (264)

Damping device to reduce the risk of injection-coupled combustion instabilities in liquid propellant rocket engines

open access: hybrid, 2020
Wolfgang Armbruster   +4 more
openalex   +1 more source

Theoretical characterization of mesoscopic structure of PBT propellant based on liquid film thickness. [PDF]

open access: yesSci Rep
Shen YW   +8 more
europepmc   +1 more source

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