Studies on Blade‐to‐Blade and Rotor‐Fuselage‐Tail Interferences

Abstract

With the increasing sophistication of modern helicopter designs the problems arising from the interactional aerodynamic flow field around the helicopter has become more acute. Interactional aerodynamics are, by origin, of utmost complexity, because many of the interactions involve viscous processes, the flow usually is unsteady and the interactions are strongly interdependent.

Citation

Huber, H. and Polz, G. (1983), "Studies on Blade‐to‐Blade and Rotor‐Fuselage‐Tail Interferences", Aircraft Engineering and Aerospace Technology, Vol. 55 No. 10, pp. 2-12. https://doi.org/10.1108/eb035904