Abstract

Present work proposed an eccentric tube-in-tube helically coiled heat exchanger (TTHC), used in Aero engine turbine film cooling which can precool compressed air more efficiently. The supercritical n-decane (3 MPa) at inner tube is used to precool the compressed air at annulus channel. The effects of mass flow rate, eccentric angle (ϕ) and eccentric ratio (e) of the inner tube on flow and heat transfer performance are investigated systematically by the RNG k−εnumerical model. The results showed that the Nusselt number (Nua) of concentric and eccentric TTHC (ϕ = 0°, e = 0.4) was 1.15 and 1.19 times of that for straight concentric tube-in-tube heat exchanger, respectively. The synergy effect at annulus side for the eccentric TTHC is more strengthened than the concentric one. When eccentric angle(ϕ) increased from 0° to 180° (e = 0.4), the Nua and fa decreased by 20% and 3%, and the performance evaluation factor (PEFa) decreased 10%. Moreover, when eccentric ratio (e) increased from 0 to 0.8 (ϕ = 0°), the Nua and the PEFa increased by 10.7% and 14%. Therefore, the optimal geometric parameters in eccentric TTHC can be selected as ϕ = 0°, e = 0.8.

Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call