LAMINAR-TURBULENT TRANSITION FOR ATTACHED AND SEPARATED FLOW

LAMINAR-TURBULENT TRANSITION FOR ATTACHED AND SEPARATED FLOW

A major challenge in the design of turbomachinery components for aircraft gas turbine engines is high cycle fatigue failures due to flutter. Of particular concern is the subsonic/transonic stall flutter boundary which occurs at part speed near the stall line. At these operating conditions the incide...

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Bibliographic Details
Main Author: Zhang, Qian
Format: Others
Published: UKnowledge 2010
Subjects:
Flutter
High Cycle Fatigue
Turbulence model
Transition model
Computational Fluid Dynamics
Aerospace Engineering
Engineering
Mechanical Engineering
Online Access:http://uknowledge.uky.edu/gradschool_diss/118
http://uknowledge.uky.edu/cgi/viewcontent.cgi?article=1122&context=gradschool_diss

Internet

http://uknowledge.uky.edu/gradschool_diss/118
http://uknowledge.uky.edu/cgi/viewcontent.cgi?article=1122&context=gradschool_diss

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