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Pourya Nikoueeyan
Pourya Nikoueeyan
Resono Pressure Systems
Verified email at resonopressuresystems.com
Title
Cited by
Cited by
Year
Global surface pressure measurements of static and dynamic stall on a wind turbine airfoil at low Reynolds number
K Disotell, P Nikoueeyan, J Naughton, G James
Experiments in Fluids 57 (5), 2016
402016
Stall flutter control of a smart blade section undergoing asymmetric limit oscillations
N Li, MJ Balas, P Nikoueeyan, H Yang, JW Naughton
Shock and Vibration 2016, 2016
192016
Characterization of the Aerodynamic Coefficients of a Wind Turbine Airfoil with a Gurney Flap for Flow Control Applications
P Nikoueeyan
32nd AIAA Applied Aerodynamics Conference, 2014
122014
Data-Driven Optimal Basis Clustering To Characterize Cycle-to-Cycle Variations in Dynamic Stall Measurements
M Ramasamy, J Wilson, P Martin, T Harms, P Nikoueeyan, J Naughton, ...
Vertical Flight Society's 75th Annual Forum & Technology Display, 2019
102019
Characterization of unsteady pressures on a blunt trailing edge using a direct-mount pressure scanner
P Nikoueeyan, M Hind, J Strike, M Singh, JW Naughton, S Keeter, ...
AIAA Scitech 2019 Forum, 1827, 2019
92019
An experimental evaluation of cycle-to-cycle variations of dynamic stall
T Harms, P Nikoueeyan, JW Naughton
2018 AIAA aerospace sciences meeting, 1267, 2018
92018
Reducing uncertainty in dynamic stall measurements through data-driven clustering of cycle-to-cycle variations
M Ramasamy, A Sanayei, JS Wilson, PB Martin, T Harms, P Nikoueeyan, ...
Journal of the American Helicopter Society 66 (1), 1-17, 2021
82021
A photogrammetric approach for masking particle image velocimetry images around moving bodies
P Nikoueeyan, JW Naughton
Measurement Science and Technology 29 (10), 105203, 2018
62018
Aerodynamic response of a wind turbine airfoil to Gurney flap deployment
P Nikoueeyan, JA Strike, AS Magstadt, M Hind, JW Naughton
33rd Wind Energy Symposium, 0995, 2015
62015
Compliance Effects in Dynamically Pitching Wind Turbine Airfoils
A Magstadt, J Strike, M Hind, P Nikoueeyan, J Naughton
31st AIAA Applied Aerodynamics Conference, 2013
62013
Evaluating the utility of pressure scanners for unsteady pressure measurements in wind tunnel characterization of the space launch system
P Nikoueeyan, MD Hind, J Strike, M Perry, B Wimpenny, L Mears, ...
AIAA AVIATION 2022 Forum, 3666, 2022
52022
Modal Analysis of the Cycle-to-Cycle Variations Observed in Dynamic Stall
T Harms, P Nikoueeyan, J Naughton
74th American Helicopter Society International Annual Forum and Technology …, 2018
52018
Quantification of uncertainty in the correction of remotely measured unsteady pressure signals on pitching airfoils
MD Hind, P Nikoueeyan, JW Naughton
33rd AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 3733, 2017
52017
Experimental assessment of an airfoil optimized to delay the onset of dynamic stall
P Nikoueeyan, T Harms, J Naughton, V Ahuja
Vertical Flight Society's 75th Annual Forum & Technology Display, 2019
42019
Unsteady Pressure Acquisition on the 1.75% Scale SLS Block 1B Cargo Liftoff Configuration
LJ Mears, PR Shea, JG Collins, MA Walker, SL Langston, JT Pinier, ...
32022
Characterization and Control of Unsteady Aerodynamics on Wind Turbine Aerofoils
J Naughton, J Strike, M Hind, A Babbitt, A Magstadt, P Nikoueeyan, ...
Journal of Physics: Conference Series 524 (1), 012025, 2014
32014
Unsteady Surface Pressures on the Space Launch System Liftoff Configuration
L Mears, PR Shea, J Collins, MA Walker, JT Pinier, P Nikoueeyan, J Strike, ...
AIAA Aviation 2022 Forum, 3667, 2022
22022
Characterizing remotely acquired pressure measurements from shock tube experiments
FA Mier, P Nikoueeyan, M Perry, M Hind, JW Naughton
AIAA SciTech 2022 Forum, 2172, 2022
22022
Photogrammetry for masking particle image velocimetry images near moving bodies
P Nikoueeyan, JW Naughton
55th AIAA Aerospace Sciences Meeting, 0941, 2017
22017
Experimental Investigation of the Structure of Turbulent Swirling Jets
E DeMillard, P Nikoueeyan, JW Naughton
54th AIAA Aerospace Sciences Meeting, 1111, 2016
22016
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