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Experimental and Computational Investigation of Divergent Thrust Losses In Rocket Nozzles
Author(s) -
Vaibhav Arya,
Anushka Sunil Kapse
Publication year - 2022
Publication title -
graduate research in engineering and technology
Language(s) - English
Resource type - Journals
ISSN - 2320-6632
DOI - 10.47893/gret.2022.1135
Subject(s) - nozzle , thrust , rocket engine , propellant , rocket (weapon) , rocket engine nozzle , aerospace engineering , mechanics , chamber pressure , characteristic velocity , discharge coefficient , combustion chamber , mechanical engineering , combustion , materials science , physics , engineering , chemistry , organic chemistry

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