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Aerothermodynamics of Gas Turbine and Rocket Propulsion, Volume 1
Gordon C. Oates
Limited preview - 1997
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12 atmospheres 90 percent n-octane approximately constant burned smoke-free burned without smoking burning nine hydrocarbon closed chamber Combustion Research Committee for Aeronautics Copies obtainable diagrs different fuel types diffusion and mixing diffusion flames E53E05 National Advisory E53E05 smoke formation effect of pressure ENCY OF DIFFUSION flow was inversely flow with pressure flowmeter formation with pressure fuel and air fuels as diffusion inversely proportional JP-4 fuel maximum relative rate maximum smoke-free fuel McDonald modified wick lamp NACA RM E53E05 National Advisory Committee nine hydrocarbon fuels obtainable from NACA Physical and Chemical pressure on smoke pressure range pressure result range the maximum rate of diffusion relative variation results indicate RM E53E05 National RM E53E05 smoke Rose Schalla and Glen September 1953 smoke-free fuel flow smoking point SMOKING TEND smoking tendency smoking was determined tabs tentatively proposed types was approximately variation in smoking variations in Copies vestigated by burning Washington NACA RM