Kenneweg, Robert; Heide, Klaas Maximilian; Böß, Volker; Denkena, Berend; Westermann, Hans-Henrik
(Berlin ; Heidelberg : Springer, 2024)
Due to impacts and constant stress, the leading edges of aircraft engine blades often lose their shape, while the other parts of the blade are still functional. This results in unnecessary performance losses. Currently, ...