Aerothermodynamics of Aircraft Engine Components (Pandora - download pdf or read online

By Gordon C. Oates

ISBN-10: 0915928973

ISBN-13: 9780915928972

Layout and R&D engineers and scholars will price the great, meticulous assurance during this quantity. starting with the elemental ideas and ideas of aeropropulsion combustion, chapters discover particular techniques, barriers, and analytical equipment as they endure on part layout.

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Additional resources for Aerothermodynamics of Aircraft Engine Components (Pandora Books)

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0039 on the shear layer mixing zone, has been shown to be successful in correlating a number of combustion characteristics ranging from exhaust pollutants to stability. A final aspect of turbulence to be discussed here involves its effect on chemical reactions. During fuel-air mixing as well as in the reaction zone, the individual turbulent eddies can have widely differing values of fuel-air ratio and temperature. Because reaction rates are very sensitive to these variables [see Eq. 4)], the turbulence characteristics can strongly influence the rates and end products of the combustion process.

13, Nos. 9-10, 1943. , Denniston, D. , and Wells, F. , 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.

21 Distillation characteristics of common jet fuels (from Ref. 29). T the initial or final temperature (approximately 298 K), and J the mechanical equivalent of heat. 6. While differences in the heats of combustion among hydrocarbons are relatively small, differences in volatility are substantial. Fuels can range from methane (boiling point of - 1 6 1 ° C ) to heavy liquid hydrocarbons containing napthalene (boiling point of 211°C). In nonaircraft turbine applications, future fuel candidates include even residual oils (which have nonvolatile components).

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Aerothermodynamics of Aircraft Engine Components (Pandora Books) by Gordon C. Oates

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