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WINGLET INSTALLATION DESIGN AND ANALYSIS
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80 PERCENT CHORD accelerometers acceptable buffet characteristics aerodynamic aileron droop back-to-back baseline aircraft basic winglet configurations BWL phase Configuration 13 CONTROL COLUMN FORCE CRUISE DRAG IMPROVEMENT cruise performance DAMPING RATIO DC-10 Series dddd Douglas Douglas Aircraft Company drag coefficient drag reduction EFFECT OF BASIC effects of winglets extended chord Flight Test Program flow separation flutter speed flutter tests FREQUENCY AND DAMPING fuel burned Ground Vibration Test inboard Krueger flap L3WER Langley Research Center leading edge device LIFT COEFFICIENT Loads Measurement LOW SPEED low-speed drag improvement lower winglet installed Mach number NASA NORMAL ACCELERATION normal force outboard ailerons predicted Pressure Distribution range factor reduced-span winglet RSWL separated flow shown in Figure spar stability and control stall speeds strain gauges test aircraft test data test results upper winglet VMIN Vortilet wind tunnel test wing bending wing box extension wing tip winglet aircraft winglet leading edge WINGLET ON LONGITUDINAL winglet span