Title: Study of the flow over a 45° sweptback wing -fuselage combination at transonic Mach numbers
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003809146&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003809146&ix=nu&I=0&V=D&pm=1</a>
Subjects: Aerodynamics, Transonic, Airplanes--Wings, Swept-back, Aerodynamics--Research.