I'm doing a survey on the topic of "gas turbine blades stress analysis" to see what areas are not focused on in this subject. I've found that not many people talk about the aerodynamic forces on the blade. Am I missing something, are they included in the calculation or are they too small to consider? Is it worth it to investigate this area? And does anyone have good resources to study in this area (papers, journals, books,...etc.) , I'm especially interested in the subject of the forces on the blade and how they are distributed. Thanks in advance.