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?

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    Just to point out, we're not a network of forums, and saying so will tend to anger people quite a bit. You'll notice that some have even incorporated the sentiment into their name as it galls so much. Jun 22 at 7:10

1 Answer 1



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 , , , 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.


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