Difficulty: Easy
Correct Answer: 10 to 15 percent
Explanation:
Introduction / Context:
Nozzle efficiency is a key parameter in turbine performance, translating enthalpy drop into kinetic energy. Surface friction and boundary-layer growth reduce the effective heat drop that converts to jet velocity, lowering the discharge speed and stage power.
Given Data / Assumptions:
Concept / Approach:
Nozzle (velocity) efficiency is typically around 0.85–0.90 for good designs. That means the actual kinetic energy at exit is 85–90% of the ideal value, implying an effective reduction in the usable heat drop of roughly 10–15%. Designers account for this when computing throat area and exit velocity from the isentropic enthalpy drop, then applying efficiency to obtain the real exit speed.
Step-by-Step Solution:
Verification / Alternative check:
Experimental nozzle tests commonly report efficiencies in the above range unless there is erosion, fouling, or severe off-design operation; these conditions could worsen losses but are not typical for design values.
Why Other Options Are Wrong:
Higher reductions (25–60%) indicate very poor nozzles or off-design shocks; not representative of standard practice.Less than 5% is overly optimistic and rarely sustained across operating ranges.
Common Pitfalls:
Confusing reduction in heat drop with reduction in velocity directly; because kinetic energy scales with velocity squared, be careful when converting between efficiency definitions and percentage speed shortfall.
Final Answer:
10 to 15 percent
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