By Gordon C. Oates
Layout and R&D engineers and scholars will price the entire, meticulous insurance during this quantity, which, below the professional editorial supervision of Gordon C. Oates, gains the invited paintings of sought after experts in plane gasoline turbine engines.
Beginning with the fundamental rules and ideas of aeropropulsion combustion, chapters discover particular approaches, boundaries, and analytical equipment as they endure on part layout.
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Additional info for Aerothermodynamics of aircraft engine components
These elements of the afterburner are illustrated in Fig. 1 for the turbojet cycle and in Fig. 2 for the turbofan cycle. The turbojet engine is a sketch of the General Electric J79 engine and the turbofan engine is a sketch of the Pratt & Whitney F100 engine. In the latter case, afterburning is accomplished without mixing core and fan streams and the inner contour of the nozzle is shown in closed (11) and open (12) positions. In both engines, a combustion chamber liner with an aircooling passage is used to protect the outer, pressure vessel wall from heat transfer by convection and radiation.
1973. CHAPTER 2. AFTERBURNERS Edward E. Zukoski California Institute of Technology, Pasadena, California 2. 1 AFTERBURNERS Introduction The simple gas turbine cycle can be designed to have good performance characteristics at a particular operating or design point. However, a particular engine does not have the capability of producing a good performance for large ranges of thrust, an inflexibility that can lead to problems when the flight program for a particular vehicle is considered. For example, many airplanes require a larger thrust during takeoff and acceleration than they do at a cruise condition.
Turbulence Effects Previous discussions of both premixed and diffusion-controlled combustion have concentrated on laminar systems. In practice, however, the presence of turbulence has an extremely important influence on both premixed and diffusion-controlled combustion. The rate of flame propagation in a premixed system is greatly enhanced by turbulence. Most available information on this subject has been developed to improve the understanding of turbulent flame propagation in afterburners. However, turbulent flame propagation information is currently of additional importance, as low-emission combustors employ a highly turbulent fuel-air mixing and vaporization zone prior to combustion (see Chap.
Aerothermodynamics of aircraft engine components by Gordon C. Oates