Arthur M. Mellor - Publications
Affiliations: | 1967 | Aerospace and Mechanical Sciences | Princeton University, Princeton, NJ |
1967-1975 | Mechanical Engineering | Purdue University, West Lafayette, IN, United States | |
1975-1988 | Mechanical Engineering | Drexel University, Philadelphia, PA, United States | |
1986-2004 | Mechanical Engineering | Vanderbilt University, Nashville, TN |
Area:
Combustion; pollutants and performance in diesel and turbine engines; hazard initiation for solid rocket propellants and explosives involving mechanical and electrostatic discharge initiationWebsite:
https://engineering.vanderbilt.edu/bio/arthur-mellorYear | Citation | Score | |||
---|---|---|---|---|---|
1976 | Tuttle JH, Shisler RA, Mellor AM. Investigation of Liquid Fueled Turbulent Diffusion Flames Combustion Science and Technology. 14: 229-241. DOI: 10.1080/00102207608547531 | 0.359 | |||
1975 | Shisler RA, Tuttle JH, Mellor AM. Emissions from and within a Film-Cooled Combustor Combustion Science and Technology. 11: 153-160. DOI: 10.1080/00102207508946694 | 0.343 | |||
1974 | Tuttle JH, Shisler RA, Mellor AM. Nitrogen dioxide formation in gas turbine engines: measurements and measurement methods Combustion Science and Technology. 9: 261-271. DOI: 10.1080/00102207408960364 | 0.38 | |||
1973 | Tuttle JH, Altenkirch RA, Mellor AM. Emissions from and within an Allison J-33 Combustor II:The Effect of Inlet Air Temperature Combustion Science and Technology. 7: 125-134. DOI: 10.1080/00102207308952350 | 0.326 | |||
1972 | Mellor AM, Anderson RD, Altenkirch RA, Tuttle JH. Emissions from and within an Allison J-33 Combustor Combustion Science and Technology. 6: 169-176. DOI: 10.1080/00102207208952318 | 0.364 | |||
1970 | Hammond DC, Mellor AM. A Preliminary Investigation of Gas Turbine Combustor Modelling Combustion Science and Technology. 2: 67-80. DOI: 10.1080/00102207008952236 | 0.377 | |||
1970 | Mellor AM, Glassman I. Augmented Ignition Efficiency for Aluminum Combustion Science and Technology. 1: 437-447. DOI: 10.1080/00102206908952224 | 0.5 | |||
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