Analysis of Factors Affecting Net Lift Increment Attainable with Trailing-Edge Split Flaps on Tailless Airplanes
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This presentation describes the interface hinge moments loads collected during the ACTE flights.
Discuss ACTE aerodynamic modeling efforts and provide comparisons of predictions to flight results for lift and pitching moment increments.
No abstract available
Longitudinal aerodynamic characteristics of semispan v/stol tilt-wing configuration with single rotating propeller
Aerodynamic characteristics determined for vertical and/or short takeoff and landing /V/STOL/ tilt-wing, multiengine aircraft
Transonic wind tunnel study of aerodynamic characteristics of blunt reentry vehicles at varying angles of attack
Longitudinal aerodynamic data on large-scale semispan V/STOL tilt-wing configuration having single propeller with left and right hand rotation