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Testing of the Trim Tab Parametric Model in NASA Langley's Unitary Plan Wind Tunnel

Karl T. Edquist, Ashley M. Korzun, Kelly J. Murphy, 2013 .

Measurement Technology for use in Active Flow Control

Richard J. Schwartz, Gary A. Fleming, Anthony N. Watkins, 2002 .

Preliminary Results from an Experimental Assessment of a Natural Laminar Flow Design Method

Sally A. Viken, Melissa B. Rivers, Richard L. Campbell, 2019, AIAA Scitech 2019 Forum.

Experimental Investigation of the NASA Common Research Model with a Natural Laminar Flow Wing in the NASA Langley National Transonic Facility

Sally A. Viken, Melissa B. Rivers, Richard L. Campbell, 2019, AIAA Scitech 2019 Forum.