This paper proposes a novel waverider generated from axisymmetric supersonic flows past
a pointed von Karman ogive. First, a pointed von Karman ogive is obtained by pointing the …

For a hypersonic gliding–cruising vehicle, the gliding Mach number is larger than the
cruising Mach number. It may be useful to design the inlet shroud to act as the compression …

View Video Presentation: https://doi. org/10.2514/6.2021-1943. vid The flow over an inclined
slender axisymmetric cylinder (L/D= 11) with an ogive forebody is investigated …

This paper describes a heuristic approach to feedback flow control and illustrates its use for
two flowfields: the flow around a tangent ogive at large angles of attack and the shear layer …

The flowfield around an axisymmetric forebody at a high angle of attack (40< α< 60 deg)
produces a significant side force. This side force results from an asymmetric pressure …

View Video Presentation: https://doi. org/10.2514/6.2021-2610. vid The aerodynamic
instability of the inclined slender cylindrical model (L/D= 11) with an ogive forebody is …

ACTIVE closed-loop flow control has shown the potential to enhance the performance of
many man-made systems involving fluid flow. However, the main stumbling block has been …

THE flow field around a slender axisymmetric forebody varies dramatically with the angle of
attack. Typically, four flow regimes are observed: attached flow (0◦≤ α< 15◦), symmetric …

The open-loop behavior of the flow actuator for the control of the asymmetric vortex at high
angle of attack are simulated using the Cobalt code. Response of the side force to various …