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- W2367341361 abstract "Aircraft with new concept rotor wing employs a high speed rotor to take off and locks the rotor to act as a fixed wing.This requires the rotor airfoil blade to be elliptic.Experimental investigation on high speed aerodynamics performance of two elliptic airfoils with 16% relative thickness and 0% and 3% relative curvature and with different camber ratio was performed in a two-dimensional testing section of FL-21 wind tunnel at China Aerodynamics Research and Development Center and TST-27 wind tunnel at Delft University Holand,respectively.The primary objects of these tests are to acquire data to validate the optimization results and develop an airfoil aerodynamic database for calculating the aerodynamic performance of this new aircraft.Techniques of measuring surface pressure and drag measurement with trail total pressure row tube were adopted.Experimental results show that the lift and pitching moment performance of cambered elliptic airfoil is better than that of the symmetrical elliptic airfoil,but the drag performance and maximum lift-drag ratio are worse than that of the symmetrical elliptic airfoil.These experimental results are valuable for the selection of main rotor wing type of this new concept aircraft." @default.
- W2367341361 created "2016-06-24" @default.
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- W2367341361 date "2009-01-01" @default.
- W2367341361 modified "2023-09-27" @default.
- W2367341361 title "Experimental Investigation on Aerodynamics Performance of Two Elliptic Airfoils at High Speed" @default.
- W2367341361 hasPublicationYear "2009" @default.
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