Difficulty: Easy
Correct Answer: Agree
Explanation:
Introduction / Context:
Nozzles are designed to convert enthalpy into directed kinetic energy. For tractable analysis and because residence times are short with insulated casings, engineers often assume adiabatic flow (Q ≈ 0). This question checks understanding of that standard assumption.
Given Data / Assumptions:
Concept / Approach:
The steady-flow energy equation reduces to h1 + V1^2/2 = h2 + V2^2/2 for adiabatic, no-work nozzles. Thus, the isentropic enthalpy drop approximates the rise in kinetic energy. While small heat losses may occur in practice, the first-order model treats the nozzle as adiabatic to predict velocities and areas accurately enough for design.
Step-by-Step Solution:
Assume Q ≈ 0 and W_s = 0; write SFEE neglecting PE change.Solve for velocity change using Δh ≈ −Δ(KE): V2^2/2 − V1^2/2 ≈ h1 − h2.Use isentropic relations to compute area–Mach numbers for given pressures.
Verification / Alternative check:
Measured nozzle efficiencies close to unity in well-designed stages justify the adiabatic approach; deviations are handled via a nozzle efficiency factor based on exit kinetic energy vs. ideal enthalpy drop.
Why Other Options Are Wrong:
“Disagree” would claim that heat transfer is essential to the model; while possible, it is secondary and usually neglected for primary sizing and performance predictions.
Common Pitfalls:
Confusing adiabatic with isentropic; adiabatic flow can still have entropy generation due to friction, so nozzle efficiency may be less than 1.
Final Answer:
Agree
Discussion & Comments