Rotor Vibratory Load Reduction by Piecewise Linear Blade Twist.

Autor:	ZHANG Yuhang, HAN Dong
Předmět:	ROTORS (Helicopters) PIECEWISE linear topology HELICOPTER rotor aerodynamics ROLLING (Aerodynamics) PITCHING moments (Aerodynamics)
Zdroj:	Transactions of Nanjing University of Aeronautics & Astronautics; Jun2024, Vol. 41 Issue 3, p278-288, 11p
Databáze:	Complementary Index
Externí odkaz:	Zobrazit plný text záznamu