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  1. Home
  2. IIT Gandhinagar
  3. Theses (PhD & Masters)
  4. Computational aero-acoustic analysis of blade-vortex interaction (BVI) in helicopter
 
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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
URI
https://d8.irins.org/handle/IITG2025/32554
Subjects
17210041
Mechanical Engineering
NACA 23012 Airfoil
Near Trailing Edge Air Suction
Vortex Diffusion
Hover Configuration
Computational Fluid Dynamics
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