1. A review of blade tip clearance–measuring technologies for gas turbine engines;Yu;Meas. Control,2020
2. A review of computational methods for aeroelastic instabilities of multi-stage compressor;Vahdati,2019
3. C. Mandache, T. Mcelhinney, N. Mrad, Aircraft engine blade tip monitoring using pulsed eddy current technology, in: 4th International Symposium on NDT in Aerospace 2012, 2012, pp. 1–12.
4. Investigation on the turbine blade tip clearance monitoring based on eddy current pulse-trigger method;Wang,2016
5. A novel blade tip clearance measurement method based on event capture technique;Wu;Mech. Syst. Signal Process.,2020