Title: Effects of compressibility on the maximum lift characteristics and spanwise load distribution of a 12-foot-span fighter-type wing of NACA 230-series airfoil sections
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003614876&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003614876&ix=nu&I=0&V=D&pm=1</a>
Subjects: Aerofoils, Compressibility, Aerodynamics--Research.