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dc.contributor.authorChandrasekhara, M.S.
dc.contributor.authorCarr, L.W.
dc.date.accessioned2016-10-03T20:17:36Z
dc.date.available2016-10-03T20:17:36Z
dc.identifier.citationM.S.Chandrasekhara, and L.W.Carr, モDesign and Development of a Facility for Compressible Dynamic Stall Studies of a Rapidly Pitching Airfoilヤ, ICIASFメ89 RECORD, IEEE Publication 89CH2762-3, pp. 29-37.
dc.identifier.urihttp://hdl.handle.net/10945/50050
dc.descriptionICIASF '89 RECORD, IEEE Publication 89CH2762-3, pp. 29-37.en_US
dc.description.abstractA facility for the study of dynamic stall of an airfoil undergoing a transient ramp type pitching motion is described. The facility can produce pitch rates of 3600 degrees/sec, to an angle of attack of 60 degrees by using a specially designed hydraulic drive with feedback control. A unique airfoil support system allows unobstructed flow visualization including the complete airfoil contour, thus permitting the use of non-intrusive optical diagnostic methods for flow measurement close to the surface as well as simultaneous far field measurements. Schlieren results obtained with this facility are presented.
dc.rightsThis publication is a work of the U.S. Government as defined in Title 17, United States Code, Section 101. Copyright protection is not available for this work in the United States.en_US
dc.titleDesign and Development of a Facility for Compressible Dynamic Stall Studies of a Rapidly Pitching Airfoilen_US
dc.typeArticleen_US
dc.description.funderAFOSR-MIPR-88-0010
dc.description.funderARO-MIPR-137-86


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