Aerodynamics: Pitching Wings
ORAL · X04 · ID: 1761506
Presentations
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Investigating the Influence of Pitch Rate and Pivot Location on Aerodynamic Performance and Leading-Edge Vortex Dynamics of Rotating and Pitching Flat Plates
ORAL
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Presenters
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Muhammad Shahan Qamar
Auburn University
Authors
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Muhammad Shahan Qamar
Auburn University
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Abbishek Gururaj
Auburn University
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Brian S Thurow
Auburn University
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Vrishank Raghav
Auburn University
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Transient Dynamics of the Flow Over a Pitching Wing at Low Reynolds Number
ORAL
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Presenters
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Connor Toppings
University of Waterloo
Authors
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Connor Toppings
University of Waterloo
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Serhiy Yarusevych
University of Waterloo
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Characterizing Dynamic Stall at High Reynolds number using a Variable Pressure Wind Tunnel
ORAL
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Presenters
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Victoria M Malarczyk
Princeton University
Authors
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Victoria M Malarczyk
Princeton University
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John W Kurelek
Princeton University
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Marcus Hultmark
Princeton University
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The Vortical Field Downstream of an Airfoil Oscillated from Rest for One Cycle
ORAL
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Presenters
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Samuel Rovani
Clarkson University
Authors
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Samuel Rovani
Clarkson University
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John T Hrynuk
DEVCOM Army Research Lab
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Douglas G Bohl
Clarkson University
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Finite-time Lyapunov exponent and force partitioning method in the wake of a pitching airfoil
ORAL
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Presenters
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Justine John A Serdoncillo
University of Minnesota
Authors
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Justine John A Serdoncillo
University of Minnesota
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Karthik Menon
Stanford University
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Melissa A Green
University of Minnesota
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2D/3D Topological data analysis of vortex dominated flows
ORAL
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Presenters
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Alemni Yiran
University of Minnesota
Authors
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Alemni Yiran
University of Minnesota
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Marko Budisic
Clarkson University
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Melissa A Green
University of Minnesota
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Rapidly pitching plates in decelerating motion near the ground.
ORAL
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Presenters
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Dibya Raj Adhikari
University of Central Florida
Authors
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Dibya Raj Adhikari
University of Central Florida
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Samik Bhattacharya
University of Central Florida
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Abstract Withdrawn
ORAL Withdrawn
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Wake dynamics of actively pitching and passively heaving tandem flappers
ORAL
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Presenters
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Chandan Bose
University of Birmingham, Assistant Professor, Aerospace Engineering, School of Metallurgy and Materials, University of Birmingham, United Kingdom
Authors
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Chandan Bose
University of Birmingham, Assistant Professor, Aerospace Engineering, School of Metallurgy and Materials, University of Birmingham, United Kingdom
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Chennakesava Kadapa
Lecturer, Mechanical Engineering, Edinburgh Napier University, United Kingdom
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Adding heterogeneous inputs to transition networks to improve unsteady airfoil lift prediction.
ORAL
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Presenters
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Ricardo Cavalcanti Linhares
University of Minnesota
Authors
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Ricardo Cavalcanti Linhares
University of Minnesota
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Karen Mulleners
EPFL, École polytechnique fédérale de Lausanne (EPFL)
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Ellen K Longmire
University of Minnesota
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Melissa A Green
University of Minnesota
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