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pro vyhledávání: '"Krenik, Alex"'
In this paper, a method is proposed to determine the flight envelope limitations for steady forward flight with the purpose of performing a flight envelope expansion. First, the rotary wing system is analyzed. In this paper, an intermeshing rotor con
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______1640::ba2a3bfec63021c2c29c90fddda0a902
https://elib.dlr.de/105053/
https://elib.dlr.de/105053/
