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TRANSITION INFORMATION

1st AIAA CFD High Lift Prediction Workshop


Image of an unstructured trap wing grid Image of a trap wing CFD solution

 

Measurements and analysis of transition on the Trap Wing (Configuration 1) were conducted (see McGinley et al, AIAA Paper 2005-5148, June 2005). For the workshop conditions the tunnel turbulence intensity was between 0.07% - 0.08% (see: 14x22-foot Tunnel Wall Information Page). The following links give some additional details and potentially helpful information:

Experimental Hot Film Locations

Experimentalist's Transition Notes

Sample Computed Transition Locations


 

Return to: Experimental Data Top Page

Return to: High Lift Prediction Workshop Home Page


 

Page Curator and NASA Official Responsible for Content
Christopher Rumsey  

Last Updated
October 14, 2011

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