Aerodynamics: Mathematical Models, Simulation and Shear Flow
ORAL · E6
Presentations
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High-order numerical simulations of the flow around wings at moderately high Reynolds number
ORAL
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Authors
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Ricardo Vinuesa
Royal Institute of Technology (KTH)
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Prabal Negi
Royal Institute of Technology (KTH)
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Seyed M. Hosseini
Royal Institute of Technology (KTH)
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Ardeshir Hanifi
Royal Institute of Technology (KTH)
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Dan Henningson
Royal Institute of Technology (KTH), KTH Stockholm
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Philipp Schlatter
Linn\'e FLOW Centre, KTH Mechanics, Linne FLOW Centre, KTH Mechanics, KTH Royal Institute of Technology, Royal Institute of Technology (KTH)
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An EnKF-based Flow State Estimator for Airfoils at High Angles of Attack
ORAL
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Authors
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Andre Fernando de Castro da Silva
California Institute of Technology
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Tim Colonius
California Institute of Technology, Caltech, Division of Engineering and Applied Science, California Institute of Technology, Pasadena, CA 91125, USA
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Mathematical Model for a Simplified Calculation of the Input Momentum Coefficient for AFC Purposes
ORAL
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Authors
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Damian Hirsch
California Institute of Technology
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Morteza Gharib
Caltech, California Institute of Technology
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Experimental Study of Thin NACA Symmetric and Cambered Airfoils at Low Reynolds Numbers
ORAL
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Authors
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Vibhav Durgesh
Cal State Univ - Northridge
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Elifalet Garcia
Cal State Univ - Northridge
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Hamid Johari
Cal State Univ - Northridge
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Lift on a Steady Airfoil in Low Reynolds Number Shear Flow
ORAL
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Authors
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Patrick Hammer
Michigan State University
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MIguel Visbal
Air Force Research Laboratory, U.S. Air Force Research Laboratory
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Ahmed Naguib
Michigan State University
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Manoochehr Koochesfahani
Michigan State University
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Experiments on a Steady Low Reynolds Number Airfoil in a Shear Flow
ORAL
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Authors
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David Olson
Michigan State University
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Ahmed Naguib
Michigan State University
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Manoochehr Koochesfahani
Michigan State University
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