Kelly Cohen

Prof. Kelly Cohen

Aerospace Engineering & Engineering Mechanics, University of Cincinnati, Cincinnati, Ohio, USA
orcid
Brian H. Rowe Endowed Chair in Aerospace Engineering & Direc...

Research Focus & Metrics

Academic Career Length

33Years (1994-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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8 August 2008 in Journal of Fluid Mechanics
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Journal Article
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SSStefan G. Siegel
Stefan G. Siegel
JSJürgen Seidel
Jürgen Seidel
CFCasey Fagley
Casey Fagley
DLD. M. Luchtenburg
D. M. Luchtenburg
Kelly CohenKelly Cohen
Kelly Cohen
TMThomas Mclaughlin
Thomas Mclaughlin
For the systematic development of feedback flow controllers, a numerical model that captures the dynamic behaviour of the flow field to be controlled is required. This poses a particular challenge for flow fields where the dynamic behaviour is nonlinear, and the governing equations cannot easily be solved in closed form. This has led to many versions of low-dimensional modelling techniques, which we extend in this work to represent better the impact of actuation on the flow. For the benchmark problem of a circular cylinder wake in the laminar regime, we introduce a novel extension to the proper orthogonal decomposition (POD) procedure that facilitates mode construction from transient data sets. We demonstrate the performance of this new decomposition by applying it to a data set from the development of the limit cycle oscillation of a circular cylinder wake simulation as well as an ensemble of transient forced simulation results. The modes obtained from this decomposition, which we refer to as the double POD (DPOD) method, correctly track the changes of the spatial modes both during the evolution of the limit cycle and when forcing is applied by transverse translation of the cylinder. The mode amplitudes, which are obtained by projecting the original data sets onto the truncated DPOD modes, can be used to construct a dynamic mathematical model of the wake that accurately predicts the wake flow dynamics within the lock-in region at low forcing amplitudes. This low-dimensional model, derived using nonlinear artificial neural network based system identification methods, is robust and accurate and can be used to simulate the dynamic behaviour of the wake flow. We demonstrate this ability not just for unforced and open-loop forced data, but also for a feedback-controlled simulation that leads to a 90% reduction in lift fluctuations. This indicates the possibility of constructing accurate dynamic low-dimensional models for feedback control by using unforced and transient forced data only.

1 January 2011 in Journal of Aerospace Information Systems
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Journal Article
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MKManish Kumar
Manish Kumar
Kelly CohenKelly Cohen
Kelly Cohen
BHBaisravan HomChaudhuri
Baisravan HomChaudhuri

1 January 2006 in Computers & Fluids
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Journal Article
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Kelly CohenKelly Cohen
Kelly Cohen
SSStefan Siegel
Stefan Siegel
TMThomas McLaughlin
Thomas McLaughlin

9 July 2015 in Unmanned Systems
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Journal Article
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NENicholas Ernest
Nicholas Ernest
Kelly CohenKelly Cohen
Kelly Cohen
EKElad Kivelevitch
Elad Kivelevitch
CSCorey Schumacher
Corey Schumacher
DCDavid Casbeer
David Casbeer

23 June 2003
Verified
Conference Paper
Closed access
SSStefan Siegel
Stefan Siegel
Kelly CohenKelly Cohen
Kelly Cohen
TMTom McLaughlin
Tom McLaughlin

2 June 2017 in Bipolar Disorders
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Journal Article
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PDF file
DFDavid E Fleck
David E Fleck
NENicholas Ernest
Nicholas Ernest
CACaleb M Adler
Caleb M Adler
Kelly CohenKelly Cohen
Kelly Cohen
JEJames C Eliassen
James C Eliassen
SSStephen M Strakowski
Stephen M Strakowski