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Flow Control on Low-Pressure Turbine Airfoils Using Vortex Generator JetsMotivation - Higher loading on Low-Pressure Turbine (LPT) airfoils: Reduce airfoil count, weight, cost. Increase efficiency, and Limited by suction side separation. Growing understanding of transition, separation, wake effects: Improved models. Take advantage of wakes. Higher lift airfoils in use. Further loading increases may require flow control: Passive: trips, dimples, etc. Active: plasma actuators, vortex generator jets (VGJs). Can increased loading offset higher losses on high lift airfoils. Objectives: Advance knowledge of boundary layer separation and transition under LPT conditions. Demonstrate, improve understanding of separation control with pulsed VGJs. Produce detailed experimental data base. Test and develop computational models.
Document ID
20100018570
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Volino, Ralph J.
(Naval Academy Annapolis, MD, United States)
Ibrahim, Mounir B.
(Cleveland State Univ. Cleveland, OH, United States)
Kartuzova, Olga
(Cleveland State Univ. Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
February 1, 2010
Publication Information
Publication: Minnowbrook VI: 2009 Workshop on Flow Physics and Control for Internal and External Aerodynamics
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Public Use Permitted.
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