Title: experimental investigation at a Mach number of 2.01 of the effects of body cross-section shape on the aerodynamic characteristics of bodies and wing-body combinations
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003853000&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003853000&ix=nu&I=0&V=D&pm=1</a>
Subjects: Airplanes--Wings, Swept-back, Aerodynamics--Research.