Global ETD Search
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Showing 1 to 3 of 3 for “"Semispan Model"”.
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Identification of Transient Nonlinear Aeroelastic Phenomena
… to a set of experiments involving a flexible semispan model (FSM) of a High Speed Civil Transport (HSCT) wing configuration conducted by Silva et al. (Experimental Steady and Unsteady Aerodynamic and Flutter Results for HSCT Semispan Models; AIAA/ASME/ASCE/AHS/ASC 41st Structures, Structural …
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The effects of aero-propulsive coupling on aircraft with distributed propulsion systems
… into the upper-surface trailing-edge of the model at the center-span location. Testing of the airfoil model was performed at Re = 1x10^6, and data were acquired as a function of angle of attack and fan speed. Force and moment data were acquired from a three-component load cell, supplemented …
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Experimental Investigation of Active Wingtip Vortex Control Using Synthetic Jet Actuators
… jet actuation (SJA) on the drag of a NACA 0015 semispan wing. The wing, which was designed and manufactured for this experiment, has an aspect ratio of 4.20, a span of 0.427 m (16.813”), and is built around an internal array of piezoelectric actuators, which work in series to create a synthetic …