Randy J. Locke
Affiliations: | 1989-1990 | APG, MD | Us Army Research Laboratory, Adelphi, MD, United States |
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Publications
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Tedder SA, Hicks YR, Locke RJ. (2013) Temperature and species measurements of combustion produced by a 9-point lean direct injector 51st Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition 2013 |
Hicks YR, Lee J, Locke RJ, et al. (2013) A study of strut based flame holder combustion physics: Comparing JP-8, JP-7, and RP-2 Fuels 8th Us National Combustion Meeting 2013. 3: 1901-1915 |
Heath CM, Hicks YR, Anderson RC, et al. (2010) Optical characterization of a multipoint lean direct injector for gas turbine combustors: Velocity and fuel drop size measurements Proceedings of the Asme Turbo Expo. 2: 791-802 |
Tacina R, Anderson R, Robinson HN, et al. (2006) Experimental performance of a swirl-venturi fuel mixer for a fuel cell reformer Proceedings of the Asme Turbo Expo. 1: 617-627 |
Gu Y, Rothe EW, Reck GP, et al. (2002) One-dimensional UV-Raman imaging of a jet-a-fueled aircraft combustor in a high temperature and pressure test cell: A feasibility study Combustion Science and Technology. 174: 199-215 |
Locke RJ, Hicks YR, Anderson RC, et al. (2002) Spontaneous raman scattering: From atmospheric CH4/air diffusion flame to 55 bar jet-a-fueled, aviation gas turbine combustor 22nd Aiaa Aerodynamic Measurement Technology and Ground Testing Conference |
Zaller M, Locke RJ, Anderson RC. (2000) Comparison of Techniques for Non-intrusive Fuel Drop Size Measurements in a Subscale Gas Turbine Combustor Journal of Visualization. 2: 301-308 |
Gu Y, Rothe EW, Reck GP, et al. (2000) 1-D, UV-Raman imaging from a high-pressure, Jet-A fueled gas turbine combustor 38th Aerospace Sciences Meeting and Exhibit |
Locke RJ, Hicks YR, Zaller MM, et al. (2000) Progress in species and flowfield mapping in advanced liquid-fueled gas turbine combustors 38th Aerospace Sciences Meeting and Exhibit |
Locke RJ, Anderson RC, Zaller MM, et al. (1998) Challenges to laser-based imaging techniques in gas turbine combustor systems for aerospace applications 20th Aiaa Advanced Measurement and Ground Testing Technology Conference |