MUMBAI, India, Sept. 14 -- Intellectual Property India has published a patent application (202541020618 A) filed by Anupama P A on March 07, 2025, for Docile Shock Control For Supercritical Airfoil.
Inventor includes Anupama P A.
The application for the patent was published on September 11, 2026, under issue no. 37/2026.
Abstract: The transition from subsonic to supersonic flow over an airfoil in the transonic regime results in substantial pressure disturbances, which give rise to shock waves and boundary layer separation. These phenomena significantly affect the aerodynamic performance of the airfoil by increasing drag and creating vortices, thus reducing lift and efficiency. To address these performance losses, flow control techniques ...