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dc.contributor.authorCarr, L.
dc.contributor.authorChandrasekhara, M.
dc.date.accessioned2017-06-02T15:49:26Z
dc.date.available2017-06-02T15:49:26Z
dc.date.issued1993
dc.identifier.citationL. Carr, M. Chandrasekhara, "Visualizing dynamic-stall airflows," NASA Tech Briefs, May 1993, 2 p.en_US
dc.identifier.urihttp://hdl.handle.net/10945/53770
dc.descriptionThis work was done by L. Carr of Ames Research Center and M. Chandrasekhara of the Naval Postgraduate School. Further information may be found in AIAA paper 89A-25511, "Design and Development of a Compression Dynamic Stall Facility".
dc.description.abstractA new wind-tunnel apparatus facilitates experiments on airfoils undergoing dynam­ic stall. Dynamic stall occurs when an airfoil is pitched rapidly past the static stall angle. In dynamic stall, lift can become greater than that in steady flow.en_US
dc.format.extent2 p.en_US
dc.publisherNASAen_US
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.titleBook Review by L. Carr and M. Chandrasekhara of Visualizing dynamic-stall airflowsen_US
dc.typeBook Reviewen_US
dc.contributor.corporateNaval Postgraduate School (U.S.)
dc.contributor.departmentAeronautics


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