G. Boxer's Applications of Engineering Thermodynamics: A tutorial text PDF

By G. Boxer

ISBN-10: 0333243544

ISBN-13: 9780333243541

ISBN-10: 134904041X

ISBN-13: 9781349040414

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Extra info for Applications of Engineering Thermodynamics: A tutorial text to Final Honours degree standard

Example text

The nozzles in the first stage of a steam turbine are fed from a steam chest of large cross-sectional area, in which the steam pressure is 110 bar and the temperature is 400 °C. 96. (b) the throat area to pass 20 kg/s of steam assuming that flow is isentropic between inlet and throat. 00141 m2 ) 14. Steam is supplied to a convergent-divergent nozzle by means of a pipe of internal diameter 120 mm. 995 dry. Calculate the pressure at the throat and the throat and exit areas required if the nozzle discharges at a pressure of 1 bar.

287 kg K where k = i' ; l 5 = 7. 86 bar 7. 54 1. _)2 · 5 = 1. 12v2 2q3 + ~ql 2q3 = 2V + Cp(Tl - T~) 2q3 kJ 300 kkJ + [ 1 . 005 'i

530v when the blower speed N is measured in rev/min and the air flow by volume v is measured in m3 /min at 1 bar and 15 °C. 78. Determine the pressure in the inlet manifold at an engine speed of 1000 rev/min given that the volumetric efficiency, based on manifold conditions, is 76% and that the blower takes in air at 1 bar and 15 °C. Also make an approximate estimate of the ratio of the indicated power of this engine to that of a similar unsupercharged engine operating at the same speed. State any assumptions made.

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Applications of Engineering Thermodynamics: A tutorial text to Final Honours degree standard by G. Boxer


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