Energy exchange in nozzles — heat transfer assumption During steady flow through a steam or gas nozzle, it is commonly assumed that no heat is supplied to or rejected by the fluid (adiabatic flow). Do you agree with this modelling assumption?

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:

  • Steady one-dimensional flow through a nozzle.
  • Insulated walls and short flow residence time.
  • No shaft work; negligible potential-energy change.


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

More Questions from Steam Nozzles and Turbines

Discussion & Comments

No comments yet. Be the first to comment!
Join Discussion