Ported shroud design of a compressor for the hydrogen reciprocating engine of a high-altitude unmanned aerial vehicle
Crossref DOI link: https://doi.org/10.1007/s12206-019-0414-y
Published Online: 2019-05-08
Published Print: 2019-05
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Jun, Sangook
Kang, Young Seok
Lim, Byeung Jun
Text and Data Mining valid from 2019-05-01
Article History
Received: 18 April 2018
Revised: 31 January 2019
Accepted: 7 February 2019
First Online: 8 May 2019