First Sentence:
The primary purpose of this introductory chapter is to discuss the main requirements of gas turbine combustors and to describe, in general terms, the various types and configurations of combustors employed in aircraft and industrial engines.
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Key Phrases - Statistically Improbable Phrases (SIPs):
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final discharge orifice, hybrid diffuser, lean blowout limits, atomizer dimensions, radial staging, initial jet angle, fuel drop size, injection pressure differential, thermoacoustic efficiency, tubular combustor, prefilming airblast atomizers, faired diffuser, weak extinction limits, large industrial engines, liner wall cooling, premix mode, prompt atomization, spray patternation, total combustor airflow, dump diffusers, effusion cooling, blowout data, combustor pattern factor, combustion oscillations, mean drop size
Key Phrases - Capitalized Phrases (CAPs):
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Journal of Engineering, Rolls Royce, New York, Dalla Betta, Dilution Jet Mixing, Journal of Fluids Engineering, Academic Press, College of Aeronautics, Conference Proceedings, Cranfield University, Air Breathing Engines, Proceedings of the Royal Society, Eighteenth Symposium, Elsevier Science, Energy Efficient Engine, London Ser, San Diego, Tenth International Symposium, Turbomachinery International, Annual Conference, Cranfield International Symposium Series, Evaluation of Fuel Character Effects, Factors Influencing Phase, Final Report, Fuel Effects
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