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Flowfield prediction of NOx and smoke production in aircraft enginesAlizadeh, Sohail January 1993 (has links)
No description available.
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The application of aero gas turbine engine monitoring systems to military aircraftBurgess, C. A. R. January 1990 (has links)
No description available.
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Study of the flowfield in the tip clearance region of compressor bladingsDoukelis, Angelos F. January 1998 (has links)
No description available.
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Smoke production in turbulent kerosene spray flames burning at elevated temperature and pressureFisher, B. A. January 1996 (has links)
No description available.
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A fast time-marching method for non-equilibrium wet steam flows in turbines ?Moheban, M. January 1983 (has links)
No description available.
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Condensation in steam turbine cascadesWhite, Alexander John January 1992 (has links)
No description available.
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Development of a modular-type computer program for the calculation of gas turbine off-design performanceMacMillan, W. L. January 1974 (has links)
This thesis presents a computer program written (in Fortran IV) to simulate the steady state off design point performance of virtually any gas turbine configuration (dealing primarily with aerospace applications). The performance is calculated using component characteristic maps for compressors, combustion chambers, turbines (both compressor turbines and free turbines) and a map giving the velocity coefficient for exhaust nozzles. The off design point performance is determined by using a modified Newton-Raphson method. Cont/d.
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An investigation into the gas dynamics of an aerovalve pulsejet engine for acoustic aerosol scavengingTaylor, Mark David January 2003 (has links)
No description available.
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An investigation into the parameters affecting the performance of a water piston engineAbdel-Gawad, T. A. K. January 1983 (has links)
No description available.
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Scale effects in small geometrically similar radial gas turbines with particular reference to bladeless volute phenomenaScrimshaw, Keith Harold January 1981 (has links)
No description available.
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