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Computational aero-acoustic analysis of blade-vortex interaction (BVI) in helicopter

Syriac, John Sherjy

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

Subjects--Topical Terms:
17210041
M.Tech
Mechanical Engineering
NACA 23012 Airfoil
Near Trailing Edge Air Suction
Vortex Diffusion
Hover Configuration
Computational Fluid Dynamics

Dewey Class. No.: 621 / SYR

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