three decades research has been carried out to explore the benefits of the mixed flow turbine in terms of lower velocity ratio operation and higher swallowing capacity [1,2,3,4]. For a non-zero rotor blade angle, the peak turbine efficiency point moves to a higher expansion ratio.
nozzle at throat Is 7mm . Calculate the number of nozzle (16) 4. Drive an expression for critical pressure ratio in terms of the index of expansion (16) 5. Explain the method of governing in steam turbine. (16)
The nozzle gas expansion process constitutes the second set of calculations. The fully reacted, equilibrated gas combustion products enter the nozzle and undergo an adiabatic expansion in the nozzle. The entropy remains constant during a reversible (isentropic) nozzle gas expansion, but in real nozzles it increases slightly.
It also won't calculate the optimum shape based on your propellant choice and flight regime; you have to figure out that stuff yourself. but you can define the ideal throat radius, and expansion ratio, and the geometry of the throat and exit nozzle size and shape will be correct for those numbers.
3.6.2 Determination of the expansion ratio (a) Apparatus: - plastic collecting vessel of volume V, approximately 500 L and accurately known to +/- 5 L; - high expansion foam-making equipment which when tested with water has a flow rate of 6.1 +/- 0.1 L/min at a nozzle pressure of (5.0 +/- 0.1) bar. An
Thus the jet noise would reflect the change in nozzle structure. Experiments with cold jet flow were conducted to explore the relationship between nozzle deformation and the spectrum pattern of jet noise. Three groups of nozzles with different expansion ratio, length of expand segment, and throat structure were used in the experiment.
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