INFLUENCE OF THE AT “WINGLETS” TYPE ON THE LONGITUDINAL STATIC STABILITY OF ANGLE OF ATTACK OF THE AIRCRAFT.

Autor:	Malikov, E., Miltsov, V.
Předmět:	VORTEX generators AERODYNAMIC load EQUATIONS of motion TORQUE ANGLE of attack (Aerodynamics) DIFFERENTIAL equations AIRPLANE wings
Zdroj:	Science-Based Technologies; 2018, Vol. 40 Issue 4, p498-505, 8p
Databáze:	Complementary Index
Externí odkaz:	Zobrazit plný text záznamu