Article citationsMore>>

A. L. Carpenter, “In-Flight Receptivity Experiments on a 30-Degree Swept-Wing Using Micron-Sized Discrete Roughness Elements,” Ph.D. Thesis, Texas A&M University, College Station, 2009.

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.