Ogive cylinders are representative designs of hypersonic forebodies and harbor several flow
complexities. This work evaluates the effects of nose bluntness of ogive-cylinder forebodies …

Impact of freestream perturbation amplitude on the flow features and dynamics of a Mach 6
flow at unit Reynolds number of 12.63× 10^ 6 1/m over a cone-cylinder-flare geometry is …

Accurate prediction of laminar to turbulent flow transition is challenging because of its
complex nature. Stability analysis has emerged as a reliable and valuable tool to identify …