Effect of intermediate aerodisk mounted sharp tip spike on the drag reduction over a hemispherical body at Mach 2.0

by Tembhurnikar Payal V., Jadhav Akash T., Sahoo Devabrata
Published 2020-01-01

Effect of vortex generator on the flow field over a conventional delta wing in subsonic flow condition at higher angles of attack

by Patil Manthan, Gawade Rajesh, Potdar Shubham, Nadaf Khushabu, Suresh Sanoj P., Sahoo Devabrata
Published 2021-01-01