Title: Theoretical investigation of the drag of generalized aircraft configurations in supersonic flow
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003874442&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003874442&ix=nu&I=0&V=D&pm=1</a>
Subjects: Drag (Aerodynamics, Aerodynamics, Supersonic, Airplanes--Design and construction.