Download Aerothermodynamics of Aircraft Engine Components (Pandora by Gordon C. Oates PDF

By Gordon C. Oates

Layout and R&D engineers and scholars will worth the excellent, meticulous insurance during this quantity. starting with the elemental rules and ideas of aeropropulsion combustion, chapters discover particular approaches, boundaries, and analytical equipment as they undergo on part layout.

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However, the first term is a very strong function of temperature and is inversely proportional to pressure because the gas density is proportional to P/T?. Hence, Eq. 6) where f increases exponentially with Tp. , by increasing the altitude at which the engine is flying, the droplet temperature must adjust to satisfy this equality. Two regimes of interest can be defined. In the first, let the gas temperature be much greater than the particle temperature. Then a drop in P~ must be accompanied by a drop in T_.

Journal of Chemical Physics, Vol. 19, 1951, p. 541. FUNDAMENTALS OF COMBUSTION 43 17Scurlock, A. C. and Grover, J. , 1953, p. 645. 18Gerstein, J. and Dugger, G. , "Turbulent Flames," Basic Considerations in the Combustion of Hydrocarbon Fuels with Air, NACA Rept. 1300, 1957, Chap. V. 19Mellor, A. , "Gas Turbine Engine Pollution," Pollution Formation and Destruction in Flames, Progress in Combustion Science and Energy, Vol. 1, edited by N. A. Chigier, 1975. 2┬░Gouldin, F. , "Controlling Emissions from Gas Turbines--The Importance of Chemical Kinetics and Turbulent Mixing," Combustion Science and Technology, Vol.

And Marble, F. , 1956, p. 205. 25Altenkirch, R. A. and Mellor, A. , 1974, pp. 1181-1189. 26Spadaccini, L. , "Autoignition Characteristics of Hydrocarbon Fuels at Elevated Temperatures and Pressures," ASME Paper 76-GT-3, 1976. 27Rao, K. V. L. and Lefebvre, A. , "Minimum Ignition Energies in Flowing Kerosene-Air Mixtures," Combustion and Flame, Vol. 27, No. 1, Aug. 1976, pp. 1-20. 2SLewis, B. , Combustion Flames and Explosions of Gases, Academic Press, New York, 1961. , 1973. CHAPTER 2. AFTERBURNERS Edward E.

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