Cal/Usaavlabs Symposium Proceedings. Aerodynamic Problems Associated with V/STOL Aircraft. Volume III. Aerodynamic Research on Boundary Layers. Held June 24, 1966, Statler-Hilton Hotel, Buffalo, New York

摘要

Contents: Spanwise flow effects on rotor performance; A preliminary study of the effect of a radial pressure gradient on the boundary layer of a rotor blade; The boundary layer of the hovering rotor; An investigation of the feasibility of a common boundary layer control system for high-lift and low-drag on an airfoil section.