Physics · Fluid Mechanics
Match the thermodynamic properties across components of a single-stage axial turbine (assuming no frictional or heat losses, and negligible radial flow):
A. Across rotor
B. Across stator
C. Across a stage
A. Across rotor
B. Across stator
C. Across a stage
Verified Solution4 OptionsUpdated: October 2026👁️1 View
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- 1A - Relative stagnation enthalpy is constant; B - Stagnation enthalpy is constant; C - Stagnation enthalpy is constant
- 2A - Stagnation enthalpy is constant; B - Stagnation enthalpy is constant; C - Enthalpy is constant
- 3A - Relative stagnation enthalpy is constant; B - None of these is constant; C - Stagnation enthalpy is constant
- 4A - Relative stagnation enthalpy is constant; B - Stagnation enthalpy is constant; C - None of these is constant✓
Correct answer
A - Relative stagnation enthalpy is constant; B - Stagnation enthalpy is constant; C - None of these is constant
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