Difficulty: Easy
Correct Answer: p2/p1
Explanation:
Introduction / Context:
The critical pressure ratio characterizes the onset of choking in compressible nozzle flow. It compares the throat static pressure at sonic conditions to the inlet (stagnation/total or chamber) pressure and determines whether further reduction in back pressure will increase mass flow.
Given Data / Assumptions:
Concept / Approach:
By convention, the critical pressure ratio is defined as the ratio of throat pressure to inlet pressure, i.e., p2/p1. For a given working fluid, this ratio has a specific value that triggers choked flow. For perfect gases it depends on the specific heat ratio; for steam, steam-table relations or empirical coefficients are used.
Step-by-Step Solution:
Identify the two pressures: p1 (inlet), p2 (throat at sonic conditions).Form the ratio as throat over inlet → p2/p1.This ratio is less than 1 and marks the limit beyond which mass flow becomes insensitive to back pressure.
Verification / Alternative check:
Performance curves display a plateau in mass flow once p_back/p1 falls below p2/p1. For air with γ = 1.4, the ideal ratio is around 0.528; steam values differ but the definition remains p2/p1.
Why Other Options Are Wrong:
Common Pitfalls:
Mixing up back pressure with critical throat pressure; the critical ratio specifically uses throat quantities at Mach 1.
Final Answer:
p2/p1
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