Zobrazeno 1 - 1
of 1
pro vyhledávání: '"flap and slat optimization"'
Design of a STOL (Short Take-Off and Landing) ultralight aircraft has been carried out at Dipartimento di Ingegneria Aerospaziale (DIAS) of University of Naples by ADAG research group. Design of the aircraft has been focused on an accurate design of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=od______3730::543ca605c0e158fe84056f07168703d4
http://hdl.handle.net/11588/117387
http://hdl.handle.net/11588/117387
