I have questions on the subject of turbomachinery -- axial compressor theory. Specifically the initial specification of stagger angle, camber angle solidity etc. of the rotor blades for a ducted fan.
Where can I ask my questions?
Meta Stack Exchange is a question and answer site for meta-discussion of the Stack Exchange family of Q&A websites. It only takes a minute to sign up.Sign up to join this community
There are many questions on the subject of fans, ducting, torque, the addition of static-blades, propeller-shape etc. on our Engineering site.
The available tags would include thrust, fluid-mechanics, aerodynamics, airflow and many others that can be seen here. You may find that a more specific search (top of the page there) than that one reveals that the answers you seek are already provided to an existing question.
You will also find that our Aviation site may provide some helpful insight into the issues you face.