Multi-stage turbocharger system analysis method for high altitude UAV engine
Crossref DOI link: https://doi.org/10.1007/s12206-017-0523-4
Published Online: 2017-07-25
Published Print: 2017-06
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Kang, Young Seok
Lim, Byeung Jun
Cha, Bong Jun
License valid from 2017-06-01
