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Supersonic Dual Bell Axisymmetric Minimum Length Nozzle Conception for High Propulsion Thrust

Crossref DOI link: https://doi.org/10.1007/s42405-019-00164-7

Published Online: 2019-03-29

Published Print: 2019-09

Update policy: https://doi.org/10.1007/springer_crossmark_policy

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