Title: Flow past a straight- and a swept-wing-body combination and their equivalent bodies of revolution at Mach numbers near 1.0
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003808476&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003808476&ix=nu&I=0&V=D&pm=1</a>
Subjects: Body of revolution, Aerodynamics--Research.