The Tip Clearance Modeling Library (TCML) was developed to model the dynamic variation of the high pressure turbine (HPT) tip clearance in aero-engine turbomachinery. The modeling techniques should be applicable to compressors as well. The model can be driven by prescribed inputs or seamlessly integrated with an aero-engine simulation such as one developed using the Toolbox for Modeling and Analysis of Thermodynamic Systems (T-MATS). - View it on GitHub