Computational aero-acoustic analysis of blade-vortex interaction (BVI) in helicopter
Source
Indian Institute of Technology, Gandhinagar
Date Issued
2019-01-01
Author(s)
Syriac, John Sherjy
Subjects
17210041
Mechanical Engineering
NACA 23012 Airfoil
Near Trailing Edge Air Suction
Vortex Diffusion
Hover Configuration
Computational Fluid Dynamics
