The effects at transonic speeds of thickening the trailing edge of a wing with a 4-percent-thick circular-arc airfoil
Description:
Report presenting an investigation of the effects of a systematic variation of trailing-edge thickness of a symmetrical, circular-arc airfoil on the aerodynamic force, moment, base-pressure, and wake fluctuations using the transonic-bump testing technique. Results regarding the effects of a systematic variation of the trailing-edge thickness, investigation of a boattailed trailing edge, and wake fluctuation characteristics are provided.
Date:
December 11, 1951
Creator:
Cleary, Joseph W. & Stevens, George L.
Item Type:
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Partner:
UNT Libraries Government Documents Department