Title: Airfoil-contour modifications based on [epsilon]-curve method of calculating pressure distribution
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003609112&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003609112&ix=nu&I=0&V=D&pm=1</a>
Subjects: Aerofoils, Aerodynamics--Research.