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Nicole L. Key, Ph.D. - Publications

Affiliations: 
2007 Mechanical Engineering Purdue University, West Lafayette, IN, United States 
Area:
Mechanical Engineering, Aerospace Engineering
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59 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2020 Leng Y, Key NL. Effects of Nonuniform Blade Spacing on Compressor Rotor Forced Response and Aeroacoustics Journal of Propulsion and Power. 36: 721-731. DOI: 10.2514/1.B37866  0.404
2020 Lou F, Key NL. Design Considerations for the Final-Stage Centrifugal Compressor in Aeroengines Journal of Propulsion and Power. 36: 791-795. DOI: 10.2514/1.B37522  0.366
2020 Gooding WJ, Fabian JC, Key NL. Laser Doppler Velocimetry Characterization of Unsteady Vaned Diffuser Flow in a Centrifugal Compressor Journal of Turbomachinery-Transactions of the Asme. 142. DOI: 10.1115/1.4046230  0.324
2020 Leng Y, Key NL. Utilization of Fast Response Pressure Measurements to Non-Intrusively Monitor Blade Vibration in Axial Compressors Journal of Turbomachinery-Transactions of the Asme. 142. DOI: 10.1115/1.4045472  0.337
2019 Lou F, Fabian JC, Key NL. Design Considerations for Tip Clearance Sensitivity of Centrifugal Compressors in Aeroengines Journal of Propulsion and Power. 35: 666-668. DOI: 10.2514/1.B37100  0.338
2019 Gooding WJ, Key NL. Leveraging LDV techniques for the investigation of unsteady turbomachinery flows Aeronautical Journal. 123: 1919-1937. DOI: 10.1017/Aer.2019.28  0.376
2018 Methel J, Smith NR, Berdanier RA, Key NL. Effects of Circumferential Nonuniformity in Compressor Flow Fields Including Vane Wake Variability Journal of Propulsion and Power. 34: 1080-1089. DOI: 10.2514/1.B36440  0.408
2018 Lou F, Fabian JC, Key NL. Interpreting Aerodynamics of a Transonic Impeller from Static Pressure Measurements International Journal of Rotating Machinery. 2018: 1-9. DOI: 10.1155/2018/7281691  0.495
2018 Gutierrez M, Petrie-Repar P, Kielb RE, Key NL. A Mistuned Forced Response Analysis of an Embedded Compressor Blisk Using a Reduced Order Model Journal of Engineering For Gas Turbines and Power-Transactions of the Asme. 141: 32505. DOI: 10.1115/1.4041280  0.32
2018 Smith NR, Key NL. A Comprehensive Investigation of Blade Row Interaction Effects on Stator Loss Utilizing Vane Clocking Journal of Turbomachinery-Transactions of the Asme. 140: 71004. DOI: 10.1115/1.4040111  0.325
2018 Li J, Aye-Addo N, Kielb R, Key NL. Mistuned Higher-Order Mode Forced Response of An Embedded Compressor Rotor, Part II: Mistuned Forced Response Prediction Journal of Turbomachinery-Transactions of the Asme. 140: 31006. DOI: 10.1115/1.4038519  0.304
2017 Berdanier RA, Smith NR, Young AM, Key NL. Effects of Tip Clearance on Stall Inception in a Multistage Compressor Journal of Propulsion and Power. 34: 308-317. DOI: 10.2514/1.B36364  0.439
2017 Berdanier RA, Key NL. Demonstrating Multistage Compressor Blockage Calculations Using Pressure Measurements for Large Tip Clearances Journal of Propulsion and Power. 34: 281-290. DOI: 10.2514/1.B36300  0.349
2017 Smith NR, Key NL. Blade-Row Interaction Effects on Unsteady Stator Loading in an Embedded Compressor Stage Journal of Propulsion and Power. 33: 248-255. DOI: 10.2514/1.B35981  0.486
2017 Lou F, Fabian JC, Key NL. Stall Inception in a High Speed Centrifugal Compressor During Speed Transients Journal of Turbomachinery-Transactions of the Asme. 139: 121004. DOI: 10.1115/1.4037759  0.323
2016 Lou F, Fabian JC, Key NL. Experimental Investigation of Flow Distortion in an Auxiliary-Power-Unit-Style Inlet System Journal of Propulsion and Power. 32: 892-902. DOI: 10.2514/1.B35948  0.427
2016 Berdanier RA, Key NL. Experimental Characterization of Tip Leakage Flow Trajectories in a Multistage Compressor Journal of Propulsion and Power. 32: 1022-1032. DOI: 10.2514/1.B35929  0.498
2016 Monk DJ, Key NL, Fulayter RD. Reduction of aerodynamic forcing through introduction of stator asymmetry in axial compressors Journal of Propulsion and Power. 32: 134-141. DOI: 10.2514/1.B35704  0.759
2016 Smith NR, Key NL. Vane Clocking Effects on Stator Suction Side Boundary Layers in a Multistage Compressor International Journal of Rotating Machinery. 2016. DOI: 10.1155/2016/5921463  0.428
2016 Bhattacharya S, Berdanier RA, Vlachos PP, Key NL. A new particle image velocimetry technique for turbomachinery applications Journal of Turbomachinery. 138. DOI: 10.1115/1.4033672  0.396
2016 Besem FM, Kielb RE, Galpin P, Zori L, Key NL. Mistuned forced response predictions of an embedded rotor in a multistage compressor Journal of Turbomachinery. 138. DOI: 10.1115/1.4032164  0.396
2016 Smith NR, Murray WL, Key NL. Considerations for measuring compressor aerodynamic excitations including rotor wakes and tip leakage flows Journal of Turbomachinery. 138. DOI: 10.1115/1.4032006  0.499
2016 Berdanier RA, Key NL. The effects of tip leakage flow on the performance of multistage compressors used in small core engine applications Journal of Engineering For Gas Turbines and Power. 138. DOI: 10.1115/1.4031625  0.507
2016 Berdanier RA, Key NL. A novel data reduction technique for single slanted hot-wire measurements used to study incompressible compressor tip leakage flows Experiments in Fluids. 57: 1-14. DOI: 10.1007/S00348-016-2114-Z  0.398
2015 Murray WL, Key NL. Experimental investigation of a forced-response condition in a multistage compressor Journal of Guidance, Control, and Dynamics. 38: 1320-1329. DOI: 10.2514/1.B35525  0.429
2015 Smith NR, Key NL. Vane clocking effects on stator loss for different compressor loading conditions Journal of Propulsion and Power. 31: 519-526. DOI: 10.2514/1.B35193  0.387
2015 Murray WL, Key NL. Detection of rotor forced response vibrations using stationary pressure transducers in a multistage axial compressor International Journal of Rotating Machinery. 2015. DOI: 10.1155/2015/198534  0.438
2015 Berdanier RA, Key NL. Experimental investigation of factors influencing operating rotor tip clearance in multistage compressors International Journal of Rotating Machinery. 2015. DOI: 10.1155/2015/146272  0.391
2015 Besem FM, Kielb RE, Key NL. Forced response sensitivity of a mistuned rotor from an embedded compressor stage Proceedings of the Asme Turbo Expo. 7. DOI: 10.1115/1.4031866  0.421
2015 Smith NR, Berdanier RA, Fabian JC, Key NL. Reconciling compressor performance differences for varying ambient inlet conditions Journal of Engineering For Gas Turbines and Power. 137. DOI: 10.1115/1.4030518  0.394
2015 Berdanier RA, Smith NR, Fabian JC, Key NL. Humidity effects on experimental compressor performance-corrected conditions for real gases Journal of Turbomachinery. 137. DOI: 10.1115/1.4028356  0.374
2015 Smith NR, Key NL. Flow visualization for investigating stator losses in a multistage axial compressor Experiments in Fluids. 56: 1-17. DOI: 10.1007/S00348-015-1964-0  0.442
2015 Lou F, Fabian J, Key NL. An experimental investigation of flow distortion in an APU-style inlet system 51st Aiaa/Sae/Asee Joint Propulsion Conference.  0.337
2015 Lou F, Murray WL, Key NL. Development of a research facility to study the flow field in an APU-style inlet 31st Aiaa Aerodynamic Measurement Technology and Ground Testing Conference.  0.338
2014 Murray WL, Key NL. Experimental investigation of a forced response condition in a multistage compressor 50th Aiaa/Asme/Sae/Asee Joint Propulsion Conference 2014. DOI: 10.2514/6.2014-3735  0.317
2014 Smith NR, Key NL. Unsteady vane boundary layer response to rotor-Rotor interactions in a multistage compressor Journal of Propulsion and Power. 30: 416-425. DOI: 10.2514/1.B34765  0.448
2014 Brossman JR, Ball PR, Smith NR, Methel JC, Key NL. Sensitivity of multistage compressor performance to inlet boundary conditions Journal of Propulsion and Power. 30: 407-415. DOI: 10.2514/1.B34742  0.752
2014 Key NL. Compressor vane clocking effects on embedded rotor performance Journal of Propulsion and Power. 30: 246-248. DOI: 10.2514/1.B34604  0.518
2014 Key NL. Influence of upstream and downstream compressor stators on rotor exit flow field International Journal of Rotating Machinery. 2014. DOI: 10.1155/2014/392352  0.475
2013 Smith NR, Key NL. Vane clocking effects on stall margin in a multistage compressor Journal of Propulsion and Power. 29: 891-898. DOI: 10.2514/1.B34636  0.412
2012 Miller KL, Key NL, Fulayter RD. Lessons learned from an aggressive outlet guide vane design for axial compressors Journal of Propulsion and Power. 28: 918-926. DOI: 10.2514/1.B34470  0.716
2012 Lou F, Fleming R, Key NL. Calculating high speed centrifugal compressor performance from averaged measurements International Journal of Turbo and Jet Engines. 29: 289-298. DOI: 10.1515/Tjj-2012-0029  0.416
2012 Brossman JR, Ball PR, Smith NR, Methel JC, Key NL. The sensitivity of multistage compressor performance to inlet boundary conditions 48th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2012.  0.721
2011 Salontay JR, Key NL, Fulayter RD. Investigation of flow physics of vane clocking effects on rotor resonant response Journal of Propulsion and Power. 27: 1001-1007. DOI: 10.2514/1.B34081  0.787
2011 Choi YS, Key N, Fleeter S. Vane clocking effects on the resonant response of an embedded rotor Journal of Propulsion and Power. 27: 71-77. DOI: 10.2514/1.48485  0.625
2011 Brossman JR, Smith NR, Talalayev A, Key NL. Tailoring inlet flow to enable high accuracy compressor performance measurements International Journal of Turbo and Jet Engines. 28: 309-320. DOI: 10.1515/Tjj.2011.065  0.758
2011 Brossman JR, Smith NR, Talalayev A, Key NL. The development of a multistage axial compressor research facility 47th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit 2011.  0.763
2010 Salontay JR, Key NL, Fulayter RD. A computational investigation of vane clocking effects on compressor forced response 48th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.  0.791
2009 Key NL, Lawless PB, Fleeter S. Vane Clocking in a Three-Stage Compressor: Frequency Domain Data Analysis Journal of Propulsion and Power. 25: 1100-1107. DOI: 10.2514/1.43423  0.648
2009 Miller KL, Key NL, Fulayter RD. Tip clearance effects on the final stage of an HPC 45th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit.  0.736
2008 Key NL, Lawless PB, Fleeter S. An investigation of the flow physics of vane clocking using unsteady flow measurements Proceedings of the Asme Turbo Expo. 6: 2003-2014. DOI: 10.1115/GT2008-51091  0.459
2008 Key NL, Lawless PB, Fleeter S. An experimental study of vane clocking effects on embedded compressor stage performance Proceedings of the Asme Turbo Expo. 6: 1973-1984. DOI: 10.1115/GT2008-51087  0.385
2008 Key NL, Lawless PB, Fleeter S. An Experimental Study of Vane Clocking Effects on Embedded Compressor Stage Performance Journal of Turbomachinery-Transactions of the Asme. 132: 11018. DOI: 10.1115/1.3072714  0.651
2007 Key NL, Lawless PB, Fleeter S. Rotor wake variability in a multistage compressor Collection of Technical Papers - 45th Aiaa Aerospace Sciences Meeting. 1: 124-135. DOI: 10.2514/1.45715  0.638
2007 Key NL, Lawless PB, Fleeter S. Vane clocking in a three-stage compressor - Frequency domain data analysis Collection of Technical Papers - 43rd Aiaa/Asme/Sae/Asee Joint Propulsion Conference. 1: 642-652.  0.349
2006 Key NL, Arts T. Comparison of turbine tip leakage flow for flat tip and squealer tip geometries at high-speed conditions Journal of Turbomachinery. 128: 213-220. DOI: 10.1115/1.2162183  0.475
2004 Key NL, Lawless PB, Fleeter S. Rotor-generated vane row off-design unsteady aerodynamics including dynamic stall, part 1 Journal of Propulsion and Power. 20: 835-841.  0.391
2002 Key NL, Lawless PB, Fleeter S. Rotor generated vane row off-design unsteady aerodynamics including dynamic stall: Part I: Stator particle image velocimetry (PIV) investigation 38th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit.  0.402
2002 Key NL. PIV study of negative incidence stator unsteady aerodynamics 40th Aiaa Aerospace Sciences Meeting and Exhibit.  0.368
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