Streamwise vortices in reattaching high-speed flows - A suggested approach

(17) The 0* at which the instability occurs is given by C = 0 and is denoted by O*.D. These values are given in Table 2 for v = 0.3 and various a/6 ratios. The corresponding classical results are given by (u/b\i = A*r/b + B*b/r Q*(r/6)/8 (18) (1 v*)(<rr)ci/E = A#(l + ?) B#(6/f)(l v) 0»»(r/6)(3 + y)/8 (19) (1 ^}Ma/E = A*(l + y) + 5*(6/r)(l p) fi*(r/6)(l + 3^)/8 (20) and applying the boundary conditions yields = crr(6)ci = 0