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Turbomachinery Isentropic Efficiency Calculator (Compressor & Turbine)

Isentropic efficiency measures the departure of actual turbomachinery from reversible adiabatic (constant entropy) compression or expansion.

Select compression or expansion process.

Fluid inlet temperature in °C.

Inlet static pressure in bar.

Outlet discharge pressure in bar.

Machine isentropic efficiency rating (typical industrial compressors ≈ 75 - 85%).

Isentropic gas exponent (Air = 1.40, Methane = 1.31, Steam = 1.30).

Calculated Result
310.1 °C

Actual Discharge Temperature

Actual Discharge Temperature

310.1°C

Ideal Isentropic Temperature

257.9°C

Pressure Ratio (P₂ / P₁)

8:1

Specific Shaft Work

291.54 kJ/kg

Isentropic Efficiency

82%

Calculation Breakdown

  1. 1. Ideal Isentropic Temperature RatioT₂s / T₁ = (P₂ / P₁)^((k-1)/k) = (8)^(0.40 / 1.4) = 1.811. T₂s = 257.9°C
  2. 2. Isentropic Efficiency CorrectionT₂_act = T₁ + (T₂s - T₁) / η = 20°C + (237.89999999999998) / 0.82 = 310.1°C
  3. 3. Specific Work CalculationW = cp · |T₂_act - T₁| = 1.005 kJ/(kg·K) · 290.1 K = 291.54 kJ/kg

Temperature and Work Profile

Interactive visualization based on your current inputs

Value
0.078156233311Inlet Temp (°C)Ideal T2s (°C)Actual T2 (°C)Work (kJ/kg)MetricValue

What Is the Turbomachinery Isentropic Efficiency Calculator (Compressor & Turbine)?

Isentropic efficiency quantifies the real-world performance of compressors and turbines relative to an ideal reversible adiabatic process.

How Does the Turbomachinery Isentropic Efficiency Calculator (Compressor & Turbine) Work?

In a Mollier h-s diagram, ideal compression follows a vertical isentropic path; real irreversible processes veer right toward higher entropy.

Turbomachinery Isentropic Efficiency Calculator (Compressor & Turbine) Formula & Variables

The core mathematical equation utilized by this calculator is expressed as:

T_{2s} = T_1 \left(\frac{P_2}{P_1}\right)^{\frac{k-1}{k}}, \quad T_{2,act} = T_1 + \frac{T_{2s} - T_1}{\eta_c}, \quad W = c_p (T_{2,act} - T_1)

Ideal isentropic discharge temperature follows the pressure ratio power law. Actual temperature accounts for efficiency losses, scaling specific work.

How to Use the Turbomachinery Isentropic Efficiency Calculator (Compressor & Turbine)

  1. Select compressor or turbine mode.
  2. Enter inlet temperature, inlet pressure, and discharge pressure.
  3. Supply isentropic efficiency percentage.

Step-by-Step Example Calculation

8:1 Pressure Ratio Air Compressor (20°C Inlet, 82% Efficiency)

Input Values:

machineType:compressor
inletTempC:20
inletPressureBar:1.0
dischargePressureBar:8.0
isentropicEfficiencyPercent:82
specificHeatRatioK:1.40
Worked Steps: Ideal isentropic temperature is 258.4°C. With 82% efficiency, actual discharge temperature rises to 311.1°C requiring 292.56 kJ/kg shaft work.

Understanding Your Result

Actual Discharge Temp: Real expected gas exit temperature.

Isentropic Temp: Minimum theoretical temperature of ideal compression.

Specific Shaft Work: Mechanical kilowatt-hours needed per kilogram fluid throughput.

Factors That Affect the Result

  • Higher pressure ratio amplifies temperature rise; lower efficiency requires proportionally higher compressor shaft power.

When Should You Use This Calculator?

  • Gas turbine power plants, turbocharger sizing, industrial air compressors, and jet engine Brayton cycle analysis.

Assumptions & Limitations

  • Assumes ideal gas behavior with constant specific heat cp over the compression temperature interval.

Frequently Asked Questions

Calculation Accuracy & Reference Note

Standard ASME PTC-10 turbomachinery thermodynamic relations.

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