MIL-PRF-23699 Thermal Diffusivity Chart

Canvas Element Not Working, Please Check Browser Settings or Contact KasperCalc to fix the issue.

Computed as α = λ/(ρ·cp) at ambient pressure. Data range: 83 °F to 158 °F (28 °C to 70 °C).

Source: NIST IR 8263 — density (Table 23), heat capacity (Table 14), thermal conductivity (Table A4).

Toggle data sets by clicking the legend.

MIL-PRF-23699 Thermal Diffusivity Calculator
Degrees (°F):
Degrees (°C):
α (m²/s):  
α (mm²/s):  
α (cm²/s):  
α (ft²/s):  
α (ft²/h):  
Thermal Diffusivity of MIL-PRF-23699 Turbine Engine Oil
About This Data

Thermal diffusivity (α) describes how quickly a material conducts heat relative to its ability to store thermal energy. It is computed from three independently measured properties: α = λ / (ρ · cp), where λ is thermal conductivity [W/(m·K)], ρ is density [kg/m³], and cp is isobaric specific heat capacity [J/(kg·K)].

The data range here is limited to 83–158 °F (28–70 °C) where all three source datasets overlap: density was measured over 5–70 °C (Table 23), specific heat capacity over 0–219 °C (Table 14), and thermal conductivity from approximately 28–226 °C (Table A4). The thermal conductivity is linearly interpolated at each temperature step.

MIL-PRF-23699 has a thermal diffusivity of roughly 8.1×10⁻⁸ m²/s near room temperature, decreasing slightly with temperature. This is an order of magnitude lower than water (~1.4×10⁻⁷ m²/s), consistent with its role as a thermal barrier lubricant rather than a coolant.

MIL-PRF-23699 — Thermal Diffusivity vs. Temperature
Temp (°C) Temp (°F) ρ (kg/m³) cp (kJ/kg·K) λ (W/m·K) α (×10⁻⁸ m²/s) α (mm²/s)

Computed: α = λ/(ρ·cp). Sources: NIST IR 8263, Tables 23, 14, A4.

Cite This Work