Boundary layer transition detection by luminescence imaging
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
2. Washington Univ., Seattle
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-177
Reference8 articles.
1. Infrared cameras for detection of boundary layer transition in transonic and subsonic wind tunnels
2. Kavandi, J.L. "Luminescence Imaging for Aerodynamic Pressure Measurements," Doctoral Thesis,Chemistry Department, Universityof Washington,1990. Summarized in Kavandi et al. "Luminescent barometry in wind tunnels," Rev. Sci. Insrum. 61(11), November 1990, pp. 3340-3347.
3. Kuethe, A.M. and Schetzer, J.P. "Foundations of Aerodynamics," 2nd editionNew York: Wiley, 1959, pp.296-297.
4. Surface pressure field mapping using luminescent coatings
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