CAL/USAAVLABS SYMPOSIUM PROCEEDINGS. AERODYNAMIC PROBLEMS ASSOCIATED WITH V/STOL AIRCRAFT. VOLUME 3. AERODYNAMIC RESEARCH ON BOUNDARY LAYERS. HELD JUNE 24, 1966, STATLER-HILTON HOTEL, BUFFALO, NEW YORK
CORNELL AERONAUTICAL LAB INC BUFFALO NY
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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.
- Fluid Mechanics