Asymmetry Features Independent of Roll Angle for Slender Circular Cone
Visualization of Vortex Flow over Delta Wing with Dorsal Fin
Pressure around a 20-degree Circular Cone at 35-degree Angle of Attack and Low Speed
Flow Control Over a Conical Forebody Using Duty-Cycled Plasma Actuators
Aerodynamic Characteristics of Slender Delta Wing with Low Dorsal Fin AIAA Paper