Shocks, Shock-Boundary Layer Interaction, And Transonic Flutter

Shocks, Shock-Boundary Layer Interaction, And Transonic Flutter

Transonic utter is an aeroelastic instability characterized by part-chord shocks over an airfoil and single mode oscillations leading to a drop in the utter boundary. We present a numerical study that examines the influence of shocks, shock-boundary layer interactions, and three-dimensional flow fea...

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Bibliographic Details
Main Author: Karnick, Pradeepa Tumkur
Other Authors: Venkatraman, Kartik
Language:en_US
Published: 2017
Subjects:
Aerodynamics
Airfoil
Transonic Flutter
Shock-Boundry Layer
Airplanes
Turbulent Viscous Flow
Flutter Boundary
Shock Dynamics
Aeroelasticity
Euler Flow
Turbulence
Transonic Flow
Aerospace Engineering
Online Access:http://etd.iisc.ernet.in/handle/2005/2688
http://etd.ncsi.iisc.ernet.in/abstracts/3509/G25863-Abs.pdf

Internet

http://etd.iisc.ernet.in/handle/2005/2688
http://etd.ncsi.iisc.ernet.in/abstracts/3509/G25863-Abs.pdf

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