Computational aero-acoustic analysis of blade-vortex interaction (BVI) in helicopter
- Gandhinagar : Indian Institute of Technology, 2019
- xv, 53p. : ill. ; 30 cm.
Including bibliography details
17210041 M.Tech Mechanical Engineering NACA 23012 Airfoil Near Trailing Edge Air Suction Vortex Diffusion Hover Configuration Computational Fluid Dynamics