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Publikováno v:
Dynamics, Vol 4, Iss 3, Pp 592-608 (2024)
The dynamic behaviour of a spring-mounted symmetrical NACA0012 wing in a freestream flow of air is studied in the pre-stall region, over 0° to 12° angles of incidence. The primary aim of this work is for use within the automotive sector to reduce d
Externí odkaz:
https://doaj.org/article/3f96b5252e404339aef285ce41d8f230