A Thermal System for Continuous Monitoring of Laminar and Turbulent Boundary-Layer Flows During Routine Flight
Description: Note presenting a thermal system which could be used to determine whether the boundary layer on a wing in flight is turbulent or laminar. Tests were made using this system in the low-turbulence pressure tunnel.
Date: September 1957
Creator: Richardson, Norman R. & Horton, Elmer A.
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