Heat exchanger testing looks simple — measure temperatures in and out. Getting accurate UA values and thermal performance maps across the operating envelope requires careful instrumentation, steady-state verification, and proper uncertainty analysis.
The Physics: Effectiveness-NTU Method
For a fuel/oil heat exchanger in aircraft applications, the effectiveness-NTU method gives the most physically meaningful performance metric.
The UA calculation begins by computing the heat capacity rates for both fluids — fuel and oil — by multiplying their respective mass flow rates by their specific heats. The algorithm identifies which fluid has the lower and higher capacity rates, then calculates the capacity ratio. The actual heat transfer rate is calculated from the fuel-side temperature rise (fuel is the cold fluid), and cross-checked against the oil-side temperature drop to verify energy balance within 2% — a balance error above that threshold flags a problem with the instrumentation or steady-state condition. The maximum possible heat transfer is the product of the minimum capacity rate and the maximum temperature difference available between the hot and cold inlets. Dividing actual by maximum heat transfer gives the effectiveness. Number of Transfer Units (NTU) is derived from effectiveness and capacity ratio using the standard NTU-effectiveness relationship for a counterflow heat exchanger, and finally UA is calculated as NTU multiplied by the minimum heat capacity rate. The result is expressed in W/K — a single number characterising the thermal conductance of the heat exchanger at that operating point.
Thermal Performance Map
Building a complete performance map means running the UA calculation at every combination of fuel flow rate, oil flow rate, and inlet temperature in the test matrix. For each test point — once steady-state is confirmed — the measured temperatures and flow rates are fed into the UA calculation to produce that point's heat transfer rate (in kW), effectiveness, and UA value. The results are compiled into a matrix indexed by fuel flow and oil flow, giving a surface that shows how the heat exchanger performs across its full operating envelope. This map is the primary deliverable for SAE ARP1827 compliance — the specification requires demonstration of thermal performance across the complete operating range, not just at a single design point.
Steady-State Verification
Never calculate UA from transient data. The acquisition system monitors temperature history over a rolling 30-second window sampled at 1 Hz. If the spread between maximum and minimum temperature readings in that window exceeds 0.1°C, the system continues waiting. Only when temperatures have been stable within that tolerance for the full window duration is the test point considered settled and data recording triggered. This prevents transient warm-up conditions, flow disturbances, or thermal lag from corrupting UA calculations — a common source of error in manual testing where an operator may record data before the system has fully stabilised.
Instrumentation Requirements
For SAE ARP1827 compliance:
- Temperature: RTD PT100 (4-wire), accuracy ±0.1°C
- Flow: Coriolis or turbine, accuracy ±0.5%
- Pressure: strain gauge transducer, accuracy ±0.1% FS
- All instruments calibrated with traceability to NIST/NPL
The Neometrix Integrated Test Rig implements this measurement chain for aircraft fuel system component testing.
→ https://neometrixgroup.com/products/integrated-test-rig-for-pumps-and-fuel-coolers
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