Centrifugal pumps have a wide range of applications in the aviation field. The present work focuses on the optimal design of aviation fuel pump impellers by means of an inverse method. The fuel pump impeller is designed here by solving an inverse problem. in which the impeller geometry is found by imposing a target blade loading. https://www.roneverhart.com/2010-FORD-FUSION-Alternator-Assembly-2-5l-125K-Miles-FWD-Automatic-Trans-G/