An Experimental and Numerical Investigation into Compressor Casing Heat Shield Effectiveness †

Journal article

An investigation was conducted into the effectiveness of heat shields in an aero-engine compressor casing to slow down thermal time constants. The investigation used a combination of experimental measurements from a full-size compressor casing rig, combined with numerical analysis using CFD and thermal modelling. Experiments were performed on a compressor casing both with and without heat shielding in order to determine the heat shield effectiveness. Temperature measurements were taken throughout the casing in order to determine the thermal time constants. The experimental data was then used to validate a thermal model and CFD simulations of the compressor casing. The modelling allowed the heat transfer coefficients in the compressor casing to be determined from the experimentally measured time constants. It was found that the heat shields gave an increase in thermal time constant at each measured location. With a doubling in the time constant at some locations compared to the unshielded case. It was also found that the heat shields need to be fully sealed, as leakage flows significantly reduce their effectiveness.

Authors: Pilkington, A; Gopalkrishna, V; Barnes, C; Lewis, L; Bacic, M

• Publication status: Published
• Peer review status: Peer reviewed
• Publisher: MDPI
• Journal: International Journal of Turbomachinery, Propulsion and Power
• Volume: 11
• Issue: 1
• Pages: 9
• Article number: 9
• Publication date: 2026-02-02
• Acceptance date: 2025-07-21
• DOI: 10.3390/ijtpp11010009
• EISSN: 2504-186X
• ISSN: 2504-186X
• Language: English
• Keywords: compressor casing; heat transfer coefficient; heat shield; thermal time constant