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The Environmental Control System is a relevant element of any conventional or More Electric Aircraft (MEA). It is either the key consumer of pneumatic power or draws a substantial load from the electric power system. The objective of this paper is to
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::fa7c7e22936e0ffc61867f61aa9b23d2
https://elib.dlr.de/73045/
https://elib.dlr.de/73045/
