Home /
Expert Answers /
Mechanical Engineering /
airfoil-analysis-this-project-consists-of-two-parts-calculating-the-airfoil-performance-and-compari-pa257
(Solved): Airfoil Analysis This project consists of two parts: calculating the airfoil performance and compari ...
Airfoil Analysis
This project consists of two parts: calculating the airfoil performance
and comparing it to the airfoil data. The airfoil and relevant wing
specifications are given below:
Use the vortex sheet analysis developed in class to
determine the following characteristics of this airfoil:
Lift-slope, a_(0)
Zero-lift angle, \alpha _(L)=0
Lift coefficient, cl at \alpha =3\deg
Moment coefficient around the quarter-chord point, c_(m,(c)/(4)) at \alpha =3\deg
Also use the boundary layer analysis developed in class to determine
Skin-friction drag coefficient, c_(d,sf)
Compare all of your results to the experimental data given at the end of this document.
