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LOWSPEED SINGLEELEMENT AIRFOIL SYNTHESIS
AN EXPLORATORY INVESTIGATION OF THE EFFECT OF A PLASTIC COATING
OPTIMUM TAIL PLANE DESIGN FOR SAILPLANES
11 other sections not shown
adverse pressure gradient aerodynamic aircraft airfoil airfoil design airfoil section airspeed altitude angle of attack applications arc wing boundary layer calculated camber chord configuration 3 plastic-coated cylinder diameter downstream downwash drag coefficient effect equation experimental flight form parameter glider high-lift in-flight computer laminar flow laminar separation bubbles leading edge Liebeck lift coefficient lift force lift-to-drag ratio loading low-drag low-speed lower surface Mach number NACA NASA netto optimized performance pilot pitch polar pressure coefficient pressure distribution pressure gradient probe profile drag propeller radial reattachment recovery region reference Reynolds number roughness element sailplane sailwing section characteristics shear layer shown in figure slipstream Soaring span speed ring stagnation pressure stall static pressure tail tests theory thermal thickness total energy sensor trailing edge transition tubing turbulent upper surface values variation variometer velocity distributions VTOL wind tunnel Wortmann zero