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A. L. Carpenter, W. S. Saric and H. L. Reed, “Roughness Receptivity in Swept-Wing Boundary Layers-Experiments,” International Journal of Engineering Systems Modeling and Simulation, Vol. 2, No. 9, 2010, pp. 128-138. doi:10.1504/IJESMS.2010.031877

has been cited by the following article:

• TITLE: Laminar-Turbulent Boundary Layer Transition Imaging Using IR Thermography

  AUTHORS: Brian K. Crawford, Glen T. Duncan Jr., David E. West, William S. Saric

  KEYWORDS: IR Thermography; Laminar; Turbulent; Transition; Flight Test; Wind Tunnel; Fluid Flow

  JOURNAL NAME: Optics and Photonics Journal, Vol.3 No.3, July 15, 2013

  ABSTRACT: Experimental techniques for imaging laminar-turbulent transition of boundary layers using IR thermography are presented for both flight and wind tunnel test environments. A brief overview of other transition detection techniques is discussed as motivation. A direct comparison is made between IR thermography and naphthalene flow visualization. A technique for obtaining quantitative transition location is presented.