The design and development of an in-draft wind tunnel test section which will be used to study the dynamic stall of airfoils oscillating in pitch is described. The hardware developed comprises a spanned airfoil between schleiren windows, a four bar linkage, flywheels, a drive system and a test section structure.
Development of Drive Mechanism for an Oscillating Airfoil
1988
9 pages
Report
Keine Angabe
Englisch
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