Published research.

Analysis of the RAFT Neural Network for Particle Image Velocimetry: Noise, Laser Sheet Effects, and Object Occlusion

Robert Whitley, Nathan Shumway, Casey Fagley, Xin Yee

AIAA SCITECH 2026 Forum (2026) · doi:10.2514/6.2026-2294

Passive Solution for Improved Stability and Drag of Cuboid Underslung Payloads

Alexandra Skeen, Luke Bradley, Antonio Tornese, Timothy M. Siefers, Casey Fagley

AIAA SCITECH 2026 Forum (2026) · doi:10.2514/6.2026-2472

Aerodynamic Evaluation of Static and Dynamic Stability Characteristics of Double-Delta Wings

Nolan A. Brody, Casey Fagley, Craig Morris

Journal of Aircraft 62(4), 949-960 (2025) · doi:10.2514/1.c038208

Comparison and Combination of Aerodynamic Data Sources for a Modern Fighter Aircraft

Spencer J. Adams, Douglas F. Hunsaker, Casey Fagley, James B. Lewis, Rick E. Graves

AIAA SCITECH 2025 Forum (2025) · doi:10.2514/6.2025-0366

Computational and Experimental Static Stability Analysis of Rectangular Prisms

Keith Bergeron, Mehdi Ghoreyshi, Casey Fagley, Timothy Siefers

Journal of Aerospace Engineering 38(2) (2025) · doi:10.1061/jaeeez.aseng-5715

Stability Augmentation on Cuboid Containers From Simple Leading Edge Modifications

David R. Johnson, Casey Fagley, Timothy M. Siefers, Keith Bergeron

AIAA SCITECH 2025 Forum (2025) · doi:10.2514/6.2025-0675

Aerodynamic Evaluation of Longitudinal and Lateral-Directional Stability Coupling on the NASA Orion Crew Module

Patrick Koenig, Joseph V. Roy, Lucas Yantis, Casey Fagley

AIAA SCITECH 2024 Forum (2024) · doi:10.2514/6.2024-0146

Aerodynamic flow field analysis of vortex interactions on multi-swept wing configurations

Mehdi Ghoreyshi, Casey Fagley, Jürgen Seidel

Aerospace Science and Technology 150, 109215 (2024) · doi:10.1016/j.ast.2024.109215

Asymmetric Vortex Breakdown on Generic Fighter Aircraft at High Angle of Attack

Nolan Brody, Casey Fagley

2024 Regional Student Conferences (2024) · doi:10.2514/6.2024-85438

Characterizing Flow Features in Responding Motion Simulations of Helicopter Sling Loads

Joy Metzler, Casey Fagley, Timothy M. Siefers, Keith Bergeron

AIAA SCITECH 2024 Forum (2024) · doi:10.2514/6.2024-1941

Computational and Experimental Static Stability Analysis of Rectangular Prisms

Ray Benson, Dylan Bumpus, Casey Fagley, Timothy M. Siefers, Mehdi Ghoreyshi, Keith Bergeron

AIAA SCITECH 2024 Forum (2024) · doi:10.2514/6.2024-0903

Journal version: doi:10.1061/jaeeez.aseng-5715

Flow Field Analysis of Vortex Interactions on Multi-Swept Wing Configurations

Christian Presas, Austin M. Park, Casey Fagley, Mehdi Ghoreyshi, Jürgen Seidel, Jacob A. Avelar

AIAA SCITECH 2024 Forum (2024) · doi:10.2514/6.2024-0904

Journal version: doi:10.1016/j.ast.2024.109215

Leading edge vortex dynamics on finite aspect ratio swept wings exhibiting large amplitude oscillations

Casey Fagley, Adam Jirasek, Jürgen Seidel

CEAS Aeronautical Journal 15(4), 999-1014 (2024) · doi:10.1007/s13272-024-00751-9

Growth, convection and breakdown of the leading-edge vortex on a swept wing in large-amplitude motion.

Wind Tunnel Evaluation of Control Effectiveness of an F-16 with a Bio-Inspired Rotating Empennage

Evan Komschlies, Casey Fagley

2024 Regional Student Conferences (2024) · doi:10.2514/6.2024-86026

Wind-tunnel forces and moments on an F-16 with a rotating horizontal tail in place of the vertical tail. Several tail angles gave lateral and directional static stability comparable to the standard F-16.

Bio-Inspired Gust Alleviation Based on Center-of-Percussion

Aidan C. Ellisor, Casey Fagley, Cale L. Franklin, Samuel P. Metzler, Samuel C. Stanton

AIAA SCITECH 2023 Forum (2023) · doi:10.2514/6.2023-0800

Experimental Investigation of the Static and Dynamic Stability Derivatives Using a Novel 3-DoF Mechanism

Jacob J. Szymanski, Casey Fagley, Molly Ellinger, Thomas Yechout

AIAA SCITECH 2023 Forum (2023) · doi:10.2514/6.2023-0799

Experimental Verification of the USAFA 1-DOF Dynamic Stability Characterization Capability and Future 3-DOF Cross Coupling Enhancements

Molly Ellinger, Jacob J. Szymanski, Casey Fagley

AIAA SCITECH 2023 Forum (2023) · doi:10.2514/6.2023-0004

Nonlinear, Rate-Dependent Evaluation of Flight Damping Derivatives of the Orion Crew Module

Casey Fagley, Robert M. Warner, Matthew R. Chmiel, Thomas R. Yechout

Journal of Spacecraft and Rockets 60(1), 239-248 (2023) · doi:10.2514/1.a35366

Forced-oscillation wind-tunnel tests of the Orion crew module give nonlinear, rate-dependent damping derivatives, and a two-degree-of-freedom model that predicts its response.

Vortex Interaction Characteristics of Multiswept Wings at Subsonic Speeds

Mehdi Ghoreyshi, Casey Fagley, Jürgen Seidel

AIAA Journal 61(7), 2932-2947 (2023) · doi:10.2514/1.j062605

Experiments on multi-swept wing planforms. The chord ratio of the first sweep strongly affects whether vortex breakdown is suppressed.

A Rate-Dependent and Time-Accurate Approach to Stability Evaluation of the NASA Orion Crew Module

Matthew R. Chmiel, Robert M. Warner, Casey Fagley, Thomas Yechout

AIAA SCITECH 2022 Forum (2022) · doi:10.2514/6.2022-0010

Conference version of the Orion crew-module study: a time-accurate method for rate-dependent damping derivatives from forced-oscillation tests.

Computational Study of Vortex Interaction Characteristics of Multi-Swept Wings at Subsonic Speeds

Mehdi Ghoreyshi, Carter c. Herman, Trevor D. Smiley, Casey Fagley, Jürgen Seidel

AIAA AVIATION 2022 Forum (2022) · doi:10.2514/6.2022-3304

Efficiency analysis of the cycloidal wave energy convertor under real-time dynamic control using a 3D radiation model

Ali Mohtat, Casey Fagley, Kedar C. Chitale, Stefan G. Siegel

International Marine Energy Journal 5(1), 45-56 (2022) · doi:10.36688/imej.5.45-56

Energy extraction by a cycloidal wave energy converter under feedback control, estimated with a control-volume model of the 3D wave field in regular, irregular and short-crested waves.

Experiments on Vortical Interactions on Generic Multi-Swept Wing Configurations

Trevor D. Smiley, Carter c. Herman, Robert M. Warner, Casey Fagley, Mehdi Ghoreyshi, Jürgen Seidel

AIAA AVIATION 2022 Forum (2022) · doi:10.2514/6.2022-3303

Force and moment, surface oil flow and stereoscopic PIV measurements on multi-swept planforms, showing how the sweep configuration drives vortex interaction and breakdown.

Numerical Evaluation of Climate Scatter Performance of a Cycloidal Wave Energy Converter

Kedar Chitale, Casey Fagley, Ali Mohtat, Stefan Siegel

International Marine Energy Journal 5(3), 315-326 (2022) · doi:10.36688/imej.5.315-326

Dynamic Stability Analysis of Bluff Body Re-Entry Vehicles using Varying Input Excitation

Matthew Robbins, Alexander Yantis, Casey Fagley, Thomas R. Yechout

AIAA Scitech 2020 Forum (2020) · doi:10.2514/6.2020-1531

Forced and free oscillation tests in the U.S. Air Force Academy subsonic wind tunnel give the pitch stability and damping of the Orion crew module and launch abort vehicle, compared with NASA data.

Distributed Propulsion Using a Wing Embedded Ejector/Diffuser

Charles F. Wisniewski, Casey Fagley

AIAA Scitech 2019 Forum (2019) · doi:10.2514/6.2019-1090

Feedback Flow Control: A Heuristic Approach

Jürgen Seidel, Casey Fagley, Thomas McLaughlin

AIAA Journal 56(10), 3825-3834 (2018) · doi:10.2514/1.j056884

A practical approach to feedback flow control, shown on a tangent ogive at high angle of attack and on the shear layer behind a backward-facing step. A wavenet ARX model with sensors at the aperture cut optical path difference by 40%.

Large Amplitude Limit Cycle Oscillations of Fully Coupled Fluid-Structure Interactions

Jürgen Seidel, Timothy M. Siefers, Casey Fagley, Thomas E. McLaughlin

2018 Fluid Dynamics Conference (2018) · doi:10.2514/6.2018-3392

Computational Study of Air Drop Control Mechanisms for Cruciform Parachutes

Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin, Greg Noetscher, Terence M. Rose

24th AIAA Aerodynamic Decelerator Systems Technology Conference (2017) · doi:10.2514/6.2017-3541

Developing a reduced order model from structural kinematic measurements of a flexible finite span wing in stall flutter

Ethan C.e. Culler, Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin, John A.n. Farnsworth

Journal of Fluids and Structures 71, 56-69 (2017) · doi:10.1016/j.jfluidstructs.2017.03.010

A reduced-order model of stall flutter built from structural measurements of a flexible wing, suitable as a basis for controller design.

Driven versus “Free Flutter” Motion of a NACA 0018 Finite Span Rigid Wing

Ethan C. Culler, John A. Farnsworth, Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin

35th AIAA Applied Aerodynamics Conference (2017) · doi:10.2514/6.2017-4359

Feedback Flow Control on a FlutteringWing using HPCMP CREATE™-AV Kestrel

Jürgen Seidel, Casey Fagley, Thomas E. McLaughlin

55th AIAA Aerospace Sciences Meeting (2017) · doi:10.2514/6.2017-0966

Modeling of transient blowing actuation using Pulse Width Modulation on a dynamically pitching NACA 0018 Airfoil

Fabien Niel, Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin

35th AIAA Applied Aerodynamics Conference (2017) · doi:10.2514/6.2017-3564

Open-Loop FLow Control on a Torsionally Flexible NACA0018 Wing

Keaton L. Turner, Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin

23rd AIAA Computational Fluid Dynamics Conference (2017) · doi:10.2514/6.2017-3615

Reduced order modeling of a dynamically pitching NACA 0018 Airfoil

Fabien Niel, Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin

55th AIAA Aerospace Sciences Meeting (2017) · doi:10.2514/6.2017-0952

Robust LQR control for stall flutter suppression: A polytopic approach

Fabien Niel, Alexandre Seuret, Luca Zaccarian, Casey Fagley

IFAC-PapersOnLine 50(1), 11367-11372 (2017) · doi:10.1016/j.ifacol.2017.08.2041

Robust LQR design for stall-flutter suppression on a NACA 0018 wing with a flap actuator, formulated with linear matrix inequalities. Simulations confirm the closed-loop behavior.

Stall Flutter Prediction and Experimental Verification using a Cyber-Physical Wing

Casey Fagley, Drew Broadbent, Jürgen Seidel, Thomas E. McLaughlin

55th AIAA Aerospace Sciences Meeting (2017) · doi:10.2514/6.2017-1416

Aero-Servo-Elastic Control of a Cyber-Physical FlexibleWing

Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin, John A. Farnsworth

54th AIAA Aerospace Sciences Meeting (2016) · doi:10.2514/6.2016-0320

Cyber-physical flexible wing for aeroelastic investigations of stall and classical flutter

Casey Fagley, Jürgen Seidel, Thomas McLaughlin

Journal of Fluids and Structures 67, 34-47 (2016) · doi:10.1016/j.jfluidstructs.2016.07.021

A wind-tunnel method that applies simulated aerodynamic loads in real time to a stationary flexible wing, so stall and flutter can be studied without flight tests.

Flow Field Analysis of Fully Coupled Computations of a Flexible Wing undergoing Stall Flutter

Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin

46th AIAA Fluid Dynamics Conference (2016) · doi:10.2514/6.2016-3632

Spanwise Variation of Stall Flutter on a Flexible NACA 0018 Finite SpanWing

Ethan C. Culler, John A. Farnsworth, Casey Fagley, Thomas E. McLaughlin

54th AIAA Aerospace Sciences Meeting (2016) · doi:10.2514/6.2016-1554

Time dependent Forcing for Flow Control on a Fluttering Wing using HPCMP CREATE™-AV Kestrel

Seidel Jürgen, Casey Fagley, Thomas E. McLaughlin

54th AIAA Aerospace Sciences Meeting (2016) · doi:10.2514/6.2016-1055

Aeroelastic Response of a Finite Span NACA 0018 Wing Part 2: Computational Simulations

Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin

53rd AIAA Aerospace Sciences Meeting (2015) · doi:10.2514/6.2015-0250

Computations of Active Open-Loop Flow Control on a Fluttering Wing

Jürgen Seidel, Casey Fagley, Thomas E. McLaughlin

33rd AIAA Applied Aerodynamics Conference (2015) · doi:10.2514/6.2015-2730

Experimental Investigation of the Aeroelastic Behavior a NACA0018 Cyber-Physical FlexibleWing

Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin

33rd AIAA Applied Aerodynamics Conference (2015) · doi:10.2514/6.2015-2251

Investigation of Aeroelastic Flow Control of a Fluttering Wing with HPCMP CREATE™-AV Kestrel

Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin

53rd AIAA Aerospace Sciences Meeting (2015) · doi:10.2514/6.2015-1505

Asymmetric Vortex State Response to Open-Loop Actuation for Variations in Angle of Attack and Reynolds Number

John A. Farnsworth, Casey Fagley, Christopher O. Porter, Thomas E. McLaughlin

52nd Aerospace Sciences Meeting (2014) · doi:10.2514/6.2014-0931

Closed-Loop Flow Control of a Forebody at a High Incidence Angle

Chris Porter, Casey Fagley, John Farnsworth, Jürgen Seidel, Thomas McLaughlin

AIAA Journal 52(7), 1430-1440 (2014) · doi:10.2514/1.j052563

Mass blowing near the nose of a forebody at high angle of attack gives a proportional side-force response. A linear model of it drives a proportional-integral law that tracks a set-point side force.

Closed-Loop Flow Control on a Ogive Forebody at a High Angle of Attack using Model Predictive Control

Christopher O. Porter, Casey Fagley, Jürgen Seidel, Thomas E. McLaughlin

52nd Aerospace Sciences Meeting (2014) · doi:10.2514/6.2014-0930

Curvature Effects of a Cycloidally Rotating Airfoil

Casey Fagley, Christopher O. Porter, Thomas E. McLaughlin

52nd Aerospace Sciences Meeting (2014) · doi:10.2514/6.2014-0255

Experimental Closed-Loop Flow Control of a von Kármán Ogive at High Incidence

Casey Fagley, Chris Porter, Thomas McLaughlin

AIAA Journal 52(12), 2891-2898 (2014) · doi:10.2514/1.j053012

3D Efficiency Analysis of Cycloidal Wave Energy Converters in Oblique Wave Fields

Casey Fagley, Stefan G. Siegel, Jürgen Seidel, Christian Schmittner

Volume 8: Ocean Renewable Energy (2013) · doi:10.1115/omae2013-10876

Closed Loop Flow Control of a Tangent Ogive at a High Angle of Attack

Christopher Porter, Casey Fagley, John Farnsworth, Jürgen Seidel, Thomas McLaughlin

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition (2013) · doi:10.2514/6.2013-395

Experimental Closed-Loop Flow Control of a von Karman Ogive at a High Angle of Attack

Casey Fagley, Christopher O. Porter, Jürgen Seidel, John A. Farnsworth, Thomas E. McLaughlin

31st AIAA Applied Aerodynamics Conference (2013) · doi:10.2514/6.2013-2924

Irregular deep ocean wave energy attenuation using a cycloidal wave energy converter

T.l. Jeans, Casey Fagley, S.g. Siegel, J. Seidel

International Journal of Marine Energy 1, 16-32 (2013) · doi:10.1016/j.ijome.2013.06.001

Novel Cyclorotor Pitching Mechanism for Operation at Curtate and Prolate Advance Ratios

Zachary Adams, Casey Fagley

51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition (2013) · doi:10.2514/6.2013-501

Numerical Simulations of Closed-Loop Flow Control of a Tangent Ogive at a High Angle of Attack

Christopher O. Porter, Casey Fagley, John A. Farnsworth, Jürgen Seidel, Thomas E. McLaughlin

31st AIAA Applied Aerodynamics Conference (2013) · doi:10.2514/6.2013-2923

Open-Loop Dynamics of the Asymmetric Vortex Wake behind a von Kármán Ogive at High Incidence

Casey Fagley, John Farnsworth, Chris Porter, Jürgen Seidel, Thomas McLaughlin, Jinik Lee, Eunseok Lee

International Journal of Flow Control 5(1), 59-78 (2013) · doi:10.1260/1756-8250.5.1.59

Plasma actuators select a port or starboard asymmetric vortex state on an ogive (fineness ratio 3.5, Reynolds number 156,000). Open-loop tests give linear models, and a PID design tracks side force in simulation.

Predictive Flow Control to Minimize Convective Time Delays

Casey Fagley, Christopher O. Porter, Thomas E. McLaughlin

AIAA Guidance, Navigation, and Control (GNC) Conference (2013) · doi:10.2514/6.2013-5016

Computational Investigation of Irregular Wave Cancelation Using a Cycloidal Wave Energy Converter

Casey Fagley, Jürgen J. Seidel, Stefan G. Siegel

Volume 7: Ocean Space Utilization; Ocean Renewable Energy 351-358 (2012) · doi:10.1115/omae2012-83434

Effects of the Plasma Actuation on the Asymmetric Vortex around an Ogive Body at High Incidence

Eunseok Lee, Jin-Ik Lee, Kwang-Seop Lee, Jürgen Seidel, Christopher Porter, Casey Fagley, Thomas McLaughlin

6th AIAA Flow Control Conference (2012) · doi:10.2514/6.2012-2954

Experimental Investigation of Irregular Wave Cancellation Using a Cycloidal Wave Energy Converter

Stefan G. Siegel, Casey Fagley, Marcus Römer, Thomas McLaughlin

Volume 7: Ocean Space Utilization; Ocean Renewable Energy 309-320 (2012) · doi:10.1115/omae2012-83388

Experimental Study of Open Loop Plasma Actuation on a von Karman Ogive

Casey Fagley, John Farnsworth, Jürgen Seidel, Tom McLaughlin

50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition (2012) · doi:10.2514/6.2012-905

Experimental wave termination in a 2D wave tunnel using a cycloidal wave energy converter

S.g. Siegel, Casey Fagley, S. Nowlin

Applied Ocean Research 38, 92-99 (2012) · doi:10.1016/j.apor.2012.07.003

Experiments in a 2D wave tunnel show a phase-controlled cycloidal rotor can cancel incoming waves.

Optimal Sensor Arrangement for Asymmetric Vortex State Estimation on a Slender Body at High Incidence

Casey Fagley, Christopher Porter, Jürgen Seidel, John Farnsworth, Thomas McLaughlin

6th AIAA Flow Control Conference (2012) · doi:10.2514/6.2012-3046

The Transient Response of a von Karman Ogive to Open Loop Plasma Actuation

John Farnsworth, Casey Fagley, Christopher Porter, Jürgen Seidel, Thomas McLaughlin

6th AIAA Flow Control Conference 42 (2012) · doi:10.2514/6.2012-2955

Vortex Dynamics of a Tangent Ogive at High Angle of Attack

Christopher Porter, Jürgen Seidel, Casey Fagley, John Farnsworth, Thomas McLaughlin

6th AIAA Flow Control Conference (2012) · doi:10.2514/6.2012-2953

Cancellation of Non-Harmonic Waves Using a Cycloidal Turbine

John T. Imamura, Stefan G. Siegel, Casey Fagley, Tom McLaughlin

Volume 5: Ocean Space Utilization; Ocean Renewable Energy 385-393 (2011) · doi:10.1115/omae2011-49262

Experimental Wave Generation and Cancellation With a Cycloidal Wave Energy Converter

Stefan G. Siegel, Marcus Ro¨mer, John Imamura, Casey Fagley, Thomas McLaughlin

Volume 5: Ocean Space Utilization; Ocean Renewable Energy 347-357 (2011) · doi:10.1115/omae2011-49212

Feedback Control of Airfoil Lift using Dense Surface Sensors and Reduced Order Models

Jürgen Seidel, Casey Fagley, Thomas McLaughlin

41st AIAA Fluid Dynamics Conference and Exhibit (2011) · doi:10.2514/6.2011-3115

Feedback Control of a Shear Layer for Aero-Optic Applications

Casey Fagley, Jürgen Seidel, Thomas McLaughlin

International Journal of Flow Control 3(1), 1-18 (2011) · doi:10.1260/1756-8250.3.1.1

A POD and wavenet model of the shear layer behind a backward-facing step is used for direct adaptive control. Simulations indicate a 35% reduction in optical aberration.

Feedback Flow Control of a Shear Layer for Aero-Optic Applications

Jürgen Seidel, Stefan Siegel, Thomas McLaughlin, Casey Fagley

48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition (2010) · doi:10.2514/6.2010-356

Journal version: doi:10.1260/1756-8250.3.1.1

Mitigation of Optical Distortions in a Free Shear Layer Using Feedback Flow Control

Jürgen Seidel, Casey Fagley, Robert Decker

2010 DoD High Performance Computing Modernization Program Users Group Conference 37, 133-138 (2010) · doi:10.1109/hpcmp-ugc.2010.12

Reduced Order Modeling Using Proper Orthogonal Decomposition (POD) and Wavenet System Identification of a Free Shear Layer

Casey Fagley, Jürgen Seidel, Stefan Siegel, Thomas McLaughlin

Notes on Numerical Fluid Mechanics and Multidisciplinary Design 325-339 (2010) · doi:10.1007/978-3-642-11735-0_21

Reduced Order Modeling for Feedback Flow Control of a Shear Layer

Jürgen Seidel, Stefan Siegel, Tom McLaughlin, Casey Fagley

5th Flow Control Conference (2010) · doi:10.2514/6.2010-4968

Structure identification in turbulent flows for feedback flow control

J Seidel, Casey Fagley, T McLaughlin

Physica Scripta T142, 014008 (2010) · doi:10.1088/0031-8949/2010/t142/014008

Surface Mounted Flow State Estimation of Reduced Order POD Models: Shear Layer

Casey Fagley, Mark Balas, Jürgen Seidel, Stefan Siegel, Thomas McLaughlin

AIAA Guidance, Navigation, and Control Conference (2010) · doi:10.2514/6.2010-7599

Reduced Order Model of Cylinder Wake with Direct Adaptive Feedback Control

Casey Fagley, Mark Balas, Stefan Siegel, Jürgen Seidel, Tom McLaughlin

AIAA Guidance, Navigation, and Control Conference (2009) · doi:10.2514/6.2009-5856

Feedback control of a circular cylinder wake

J Seidel, S Siegel, Casey Fagley, K Cohen, T McLaughlin

Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering 223(4), 379-392 (2008) · doi:10.1243/09544100jaero407

Low-dimensional modelling of a transient cylinder wake using double proper orthogonal decomposition

Stefan G. Siegel, Jürgen Seidel, Casey Fagley, D. M. Luchtenburg, Kelly Cohen, Thomas McLaughlin

Journal of Fluid Mechanics 610, 1-42 (2008) · doi:10.1017/s0022112008002115

A double-POD method that builds flow modes from transient data, shown on the flow behind a circular cylinder. Fagley is a co-author; the first author is S. G. Siegel.

Reduced Order Model Based Control of Large Scale Aero-Elastic Simulations

Casey Fagley, Mark Balas

AIAA Guidance, Navigation and Control Conference and Exhibit (2008) · doi:10.2514/6.2008-6965

Wave Estimation Tool v1.1 - LSTM + Space-Time POD

A PyTorch and Streamlit tool that predicts wave elevation seconds ahead from upstream sensors. Supports Airy, Stokes, JONSWAP and Bretschneider spectra and exports to LabVIEW real-time targets.

Client software, listed for completeness. No public DOI.

Comparison of driven and simulated ``free'' stall flutter in a wind tunnel

Ethan C.e. Culler, John Farnsworth, Casey Fagley, Jürgen Seidel

Bulletin of the American Physical Society (2016)

Detection and estimation of the instantaneous flow topology on an airfoil using proper orthogonal decomposition

Jürgen Seidel, Casey Fagley, Tom McLaughlin

Bulletin of the American Physical Society 63 (2010)

Open Loop Forced Experimental Investigation of Optical Beam Propagation through a Free Shear Layer

Casey Fagley, Stefan Siegel, Jürgen Seidel, Thomas McLaughlin

Bulletin of the American Physical Society 62 (2009)

Experimental Investigation of Optical Beam Propagation through a free Shear Layer

Stefan Siegel, Juergen Seidel, Casey Fagley, Thomas McLaughlin

Bulletin of the American Physical Society 61 (2008)

Reduced Order Modeling for Beam Propagation through a Shear Layer

Jürgen Seidel, Casey Fagley, Stefan Siegel, Thomas McLaughlin

Bulletin of the American Physical Society 61 (2008)