Title: Flight investigation of boundary-layer transition and profile drag of an experimental low-drag wing installed on a fighter-type airplane
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003613553&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003613553&ix=nu&I=0&V=D&pm=1</a>
Subjects: Airplanes--Control surfaces, Aerofoils, Aerodynamics--Research.