Aerodynamics: Fixed, Flapping and Rotating Wing II
ORAL · H25 · ID: 22707
Presentations
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Unsteady forces on the wing subjected to spanwise twisting
ORAL
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Presenters
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Kamlesh Joshi
Authors
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Kamlesh Joshi
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samik bhattacharya
University of Central Florida
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Determination of Flow Field Parameters using Inverse Interpolation Methods
ORAL
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Presenters
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Sruthi Chengalrayan
University of Arizona
Authors
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Sruthi Chengalrayan
University of Arizona
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Kyle M Hanquist
University of Arizona
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Sergey V Shkarayev
University of Arizona
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Investigation of surface pressure fluctuations in airfoils subject to transverse gust: towards gust mitigation
ORAL
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Presenters
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Ioannis M Mandralis
California Institute of Technology, Caltech
Authors
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Ioannis M Mandralis
California Institute of Technology, Caltech
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H. Jane Bae
California Institute of Technology, Caltech
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Unsteady Evolution of a Laminar Separation Bubble Subjected to Wing Structural Motion
ORAL
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Presenters
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Adrian Grille guerra
TU Delft
Authors
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Adrian Grille guerra
TU Delft
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Shirzad Hosseinverdi
University of Arizona
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Jesse C Little
University of Arizona
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Hermann F Fasel
University of Arizona
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Impact of Surging Streamwise Flow on Laminar Separation Bubble Dynamics for a Finite-Span Wing
ORAL
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Presenters
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Dasha Gloutak
University of Colorado, Boulder
Authors
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Dasha Gloutak
University of Colorado, Boulder
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John A Farnsworth
University of Colorado, Boulder
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An inverted wing in extreme ground effect produces downforce with a static peak at h/c~10%. A sinusoidally heaving wing at reduced frequency of k=0.5 has less average downforce than the static mean. Dynamic downforce is approximated from analytical/state-space models based on static chordwise separation.
ORAL
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Publication: Jacuzzi, E., Granlund, K., 2020, "Heaving Inverted Wing in Extreme Ground Effect," Journal of Fluids Engineering, Volume 142(11) https://doi.org/10.1115/1.4047804.
Presenters
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Eric A Jacuzzi
Authors
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Eric A Jacuzzi
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Kenneth Granlund
North Carolina State University
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Visualization and Transport Analysis of Non-slender Delta Wing Vortices
ORAL
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Presenters
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Mohammad Elsouht
The University of Iowa
Authors
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Mohammad Elsouht
The University of Iowa
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James H Buchholz
University of Iowa
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Proper Orthogonal Decomposition of NACA-0012 in the Wake of a Square Bluff Body
ORAL
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Presenters
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Rodrigo Padilla
University of Idaho
Authors
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Rodrigo Padilla
University of Idaho
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Vibhav Durgesh
University of Idaho
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Wake bi-modal switching and its dependence on the upstream bluff body boundary layers
ORAL
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Publication: Ahmed, D. and Morgans, A., 2021, "Wake Bi-modality: the effect of the upstream separation bubble",(In progress).
Presenters
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Dania Ahmed
Imperial College London
Authors
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Dania Ahmed
Imperial College London
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Aimee Morgans
Imperial College London
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Wake of an Oscillating Cylinder in Noisy Flow
ORAL
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Presenters
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Kumar Sourav
Indian Institute of Technology Madras, Chennai-600036, Tamil Nadu, India
Authors
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Kumar Sourav
Indian Institute of Technology Madras, Chennai-600036, Tamil Nadu, India
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Sunetra Sarkar
Department of Aerospace Engineering, Indian Institute of Technology Madras (IITM), Chennai-600036, Tamil Nadu, India., Indian Institute of Technology Madras, Chennai-600036, Tamil Nadu, India
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