Tutorial for XFoil
This will display the minimum Cp distribution. Minimum Inviscid Cp =-17.2591 at x = 0.0004. Minimum Viscous Cp =-12.1387 at x = 0.0010. Type.OPERv c> cpmi -18. To re-plot the Cp distribution type.OPERv c> cpx. The Cp distribution should now look like this: Figure 4. Flow Around an Airfoil at a High Alpha. Saving the Cp Distribution to a File ................
................
To fulfill the demand for quickly locating and searching documents.
It is intelligent file search solution for home and business.
Related searches
- salesforce lightning tutorial for beginners
- onenote tutorial for beginners
- free excel tutorial for beginners
- excel tutorial for beginners pdf
- onenote 2016 tutorial for beginners
- minecraft tutorial for beginners
- fractions tutorial for adults
- email tutorial for beginners pdf
- onenote 2010 tutorial for beginners
- network tutorial for beginners pdf
- networking tutorial for beginners
- computer tutorial for beginners