Question #56280
Using XFLR5
Based on a CL vs Alpha and on a CD vs Alpha:If an airfoil flies upside down, what is the maximum lift, and at what angle?
How can am i suppose to find that out from those two graphs provided by XFLR5 ?
Based on a CL vs Alpha and on a CD vs Alpha:If an airfoil flies upside down, what is the maximum lift, and at what angle?
How can am i suppose to find that out from those two graphs provided by XFLR5 ?
Expert's answer
Answer in progress...
Learn more about our help with Assignments: Engineering
Comments