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pro vyhledávání: '"Hua Cheng Tao"'
Publikováno v:
Applied Mechanics and Materials. :587-592
According to the fact that it need several tests to determine the size and motion parameters of the flapping-wing aircraft in the development processes, the paper proposed a design scheme of flapping wing system experimental platform. Separately from
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cef48706ce9f32e2be336db701ee7248
https://doi.org/10.4028/www.scientific.net/amm.651-653.587
https://doi.org/10.4028/www.scientific.net/amm.651-653.587
