Zobrazeno 1 - 3
of 3
pro vyhledávání: '"Liuyue Bai"'
Publikováno v:
Aerospace, Vol 10, Iss 10, p 870 (2023)
Due to the maneuver and overload requirements of aircraft, it is inevitable that supersonic fins experience high angles of attack (AOAs) and viscous effects at high altitudes. The local piston theory with viscous correction (VLPT) is introduced and m
Externí odkaz:
https://doaj.org/article/48e5d3dbbf6643788d1c0a3f84ed1a9c
Publikováno v:
Applied Sciences, Vol 13, Iss 3, p 1262 (2023)
Establishing the aeroelastic characteristic of all-movable fins with freeplay nonlinearities is one of the most common problems in the design of supersonic flight vehicles. In this context, this study provided novel points of view on the nonlinear ae
Externí odkaz:
https://doaj.org/article/b55a7aa1919d40a0818689cabbd6c2d4
Publikováno v:
Applied Sciences (2076-3417); Feb2020, Vol. 10 Issue 4, p1205, 17p