Dynamic stability and control laws of a hingeless rotor helicopter were studied.
研究了无铰直升机动稳定性、操纵性和控制问题。
The experimental results verify that the feasible theory can be used to investigate the effects of structural parameters of hingeless rotor on aeroelastic stability.
Through comparative study of hingeless arch bridge , two-hinged arch bridge and three-hinged arch bridge, the influence of connection condition of arch on mechanical condition is discussed.