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S. Zuccher and W. S. Saric, “Infrared Thermography Investigations in Transitional Supersonic Boundary Layers,” Experiments in Fluids, Vol. 44, 2008, pp. 145-157.
doi:10.1007/s00348-007-0384-1
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[2]
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W. S. Saric, H. L. Reed and D. W. Banks, “Flight Testing of Laminar Flow Control in High-Speed Boundary Layers,” The RTO Applied Vehicle Technology Panel (AVT) Specialists’ Meeting, Prague, 4-7 October 2004.
http://www.cso.nato.int/Main.asp?topic=5
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[3]
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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
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D. Arnal and J. P. Archambaud, “Laminar-Turbulent Transition Control: NLF, LFC, HLFC,” Advances in Laminar-Turbulent Transition Modeling, VKI Lecture Series, Brussels, 2008.
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[5]
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D. N. Mavris, W. S. Saric, H. Ran, M. J. Belisle, M. J. Woodruff and H. L. Reed, “Investigation of a Health Monitoring Methodology for Future Natural Laminar Flow Transport Aircraft,” ICAS Paper 1.9.3, Nice, 2010.
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[6]
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K. L. Chapman, M. S. Reibert, W. S. Saric and M. N. Glauser, “Boundary-Layer Transition Detection and Structure Identification through Surface Sheer-Stress Measurements,” Proceedings of the 36th AIAA Aerospace Sciences Meeting and Exhibit, Reno, 12-15 January 1998.
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[7]
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A. Ahmed, W. H. Wentz Jr. and R. Nyenhuis, “Natural Laminar Flow Flight Experiments on a Swept-Wing Business Jet,” Proceedings of the AIAA 2nd Applied Aero dynamics Conference, Seattle, 21-23 August 1984.
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A. Drake, “Oil Film Interferometry for Boundary Layer Measurements in Aircraft Development,” Proceedings of the 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, Portland, 28 June-1 July 2004. doi:10.2514/6.2004-2114
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[9]
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M. McQuilling, M. Wolff, S. Fonov, J. Crafton and R. Sondergaard, “An Experimental Investigation of Low Pressure Turbine Blade Suction Surface Stresses Using S3F,” Proceedings of the 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, 2006.
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[10]
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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.
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[11]
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G. T. Duncan Jr., B. K. Crawford and W. S. Saric, “Flight Experiments on the Effects of Step Excrescences on Swept-Wing Transition,” Proceedings of the 48th Applied Aerodynamics Symposium, Saint-Louis, 25-27 March 2013.
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