Title: Drag reduction by suction of the boundary layer separated behind shock wave formation at high mach numbers
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003760239&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003760239&ix=nu&I=0&V=D&pm=1</a>
Subjects: Drag (Aerodynamics, Boundary layer.