Air Vehicle Aerodynamics
ORAL · G16
Presentations
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High Speed Focused Schlieren Flow Visualization of Shock Induced Dynamic Stall
ORAL
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Authors
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Patrick Bowles
University of Notre Dame
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Dustin Coleman
University of Notre Dame
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Thomas Corke
University of Notre Dame
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Flint Thomas
University of Notre Dame
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Mark Wasikowski
Bell Helicopter
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Boundary Layer Trip Effects On Incipient Dynamic Stall Flutter
ORAL
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Authors
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Thomas Corke
University of Notre Dame
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Patrick Bowles
University of Notre Dame
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Dustin Coleman
University of Notre Dame
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Flint Thomas
University of Notre Dame
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Mark Wasikowski
Bell Helicopter
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Velocity measurements in the near wake of a ship superstructure
ORAL
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Authors
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Cody Brownell
U.S. Naval Academy
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Luksa Luznik
Mechanical Engineering Department, US Naval Academy, U.S. Naval Academy
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Murray Snyder
U.S. Naval Academy
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Hyung Suk Kang
U.S. Naval Academy
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Colin Wilkinson
Zenetex LLC
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Energy Exchange during Plunge/Surge Motions of a 2D Wing
ORAL
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Authors
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Wesley Kerstens
Illinois Institute of Technology
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Jeesoon Choi
California Institute of Technology
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Tim Colonius
California Institute of Technology, Division of Engineering and Applied Science, California Institute of Technology
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David Williams
Illinois Institute of Technology
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Facility Dependent Issues Influencing the Experimental Characterization of a Laminar Separation Bubble
ORAL
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Authors
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David A. Olson
Michigan State University
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Ahmed M. Naguib
Michigan State University, Mechanical Engineering, Michigan State University, Department of Mechanical Engineering, Michigan State University
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Manoochehr M. Koochesfahani
Michigan State University
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Experimental Investigation of Tip Vortex Control Using a Half-Delta Shaped Tip Strake
ORAL
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Authors
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Jennifer Pereira
McGill University
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Drag reduction in large wind turbines through riblets: evaluation of different geometries
ORAL
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Authors
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Roger Arndt
University of Minnesota, Dept of Civil Engineering, UMN
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Leonardo Chamorro
University of Minnesota, SAFL, Dep. Civil Engineering, University of Minnesota, MN, Dept of Civil Engineering, UMN
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Fotis Sotiropoulos
St. Anthony Falls Laboratory, University of Minnesota, University of Minnesota, Univ. of Minnesota, Dept of Civil Engineering, UMN, St. Anthony Falls Laboratory, Department of Civil Engineering, 2 Third Avenue SE, Minneapolis, MN 55414, USA
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Aerodynamic Behavior at One Revolution Angle of Attack of Two-Dimensional Wings
ORAL
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Authors
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Yong Oun Han
School of Mechanical Engineering, Yeungnam University
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Eun Ha Lee
Graduate Student
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Jeong Hyun Kim
Research Associate
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Yong Oh Shin
WESTEC
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Electro-Luminescence based Pressure-Sensitive Paint System for Unsteady Flow Field Measurements
ORAL
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Authors
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Hirotaka Sakaue
Japan Aerospace Exploration Agency
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Yoshimi Iijima
Aerospace Research and Development Directorate, JAXA
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