| Effects of boundary-layer ingestion on the aero-acoustics of transonic fan rotors JJ Defoe, ZS Spakovszky Journal of Turbomachinery 135 (5), 051013, 2013 | 40 | 2013 |
| Fan performance scaling with inlet distortions JJ Defoe, M Etemadi, DK Hall Journal of Turbomachinery 140 (7), 071009, 2018 | 38 | 2018 |
| A novel mpt noise methodology for highly-integrated propulsion systems with inlet flow distortion J Defoe, A Narkaj, Z Spakovszky 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference …, 2009 | 22 | 2009 |
| Shock propagation and mpt noise from a transonic rotor in nonuniform flow JJ Defoe, ZS Spakovszky Journal of Turbomachinery 135 (1), 011016, 2013 | 17 | 2013 |
| A body-force based methodology for predicting multiple-pure-tone noise: Validation J Defoe, A Narkaj, Z Spakovszky 16th AIAA/CEAS Aeroacoustics Conference, 3747, 2010 | 16 | 2010 |
| Scaling of incidence variations with inlet distortion for a transonic axial compressor DJ Hill, JJ Defoe Journal of Turbomachinery 142 (2), 021003, 2020 | 12 | 2020 |
| Innovations in body force modeling of transonic compressor blade rows DJ Hill, JJ Defoe International Journal of Rotating Machinery 2018 (1), 6398501, 2018 | 12 | 2018 |
| Prediction of crosswind separation velocity for fan and nacelle systems using body force models: Part 2: Comparison of crosswind separation velocity with and without detailed … QJ Minaker, JJ Defoe International Journal of Turbomachinery, Propulsion and Power 4 (4), 41, 2019 | 10 | 2019 |
| A new loss generation body force model for fan/compressor blade rows: an artificial-neural-network based methodology S Pazireh, JJ Defoe International Journal of Turbomachinery, Propulsion and Power 6 (1), 5, 2021 | 8 | 2021 |
| Prediction of crosswind separation velocity for fan and nacelle systems using body force models: Part 1: Fan body force model generation without detailed stage geometry QJ Minaker, JJ Defoe International Journal of Turbomachinery, Propulsion and Power 4 (4), 43, 2019 | 8 | 2019 |
| A new loss generation body force model for fan/compressor blade rows: application to uniform and non-uniform inflow in rotor 67 S Pazireh, J Defoe Journal of Turbomachinery 144 (6), 061005, 2022 | 7 | 2022 |
| Inlet swirl distortion effects on the generation and propagation of fan rotor shock noise JJJ Defoe Massachusetts Institute of Technology, 2011 | 7 | 2011 |
| A Novel Numerical Approach for Generation and Propagation of Rotor-Stator Interaction Noise K Patel, C Novak, J Defoe 22nd AIAA/CEAS Aeroacoustics Conference, 2821, 2016 | 6 | 2016 |
| An investigation of nonlinear flow oscillations in a high-pressure centrifugal pump C Lettieri, J Defoe, ZS Spakovszky Journal of Turbomachinery 137 (11), 111004, 2015 | 6 | 2015 |
| The effect of blade count on body force model performance for axial fans P Saini, J Defoe Journal of Turbomachinery 143 (7), 071011, 2021 | 5 | 2021 |
| Review of computational aeroacoustics for application in electronics cooler noise J Defoe, C Novak Canadian Acoustics 34 (3), 76-77, 2006 | 5 | 2006 |
| A no-calibration approach to modelling compressor blade rows with body forces employing artificial neural networks S Pazireh, JJ Defoe Turbo Expo: Power for Land, Sea, and Air 58554, V02AT39A013, 2019 | 4 | 2019 |
| A critical analysis of loudness calculation methods JJ Defoe, CJ Novak, HJ Ule, RG Gaspar Canadian Acoustics 35 (1), 25-33, 2007 | 3 | 2007 |
| Evaluation of loudness calculation techniques with applications for product evaluation J Defoe University of Windsor, 2007 | 3 | 2007 |
| Assessment of Fan Stall Point Identification Ability of Steady RANS Computations With the Helicity-Corrected Spalart-Allmaras Turbulence Model Z Yu, H Raza, J Defoe Turbo Expo: Power for Land, Sea, and Air 87103, V13CT32A039, 2023 | 2 | 2023 |
Zoltan SpakovszkyProfessor of Aeronautics and Astronautics, MIT在 mit.edu 的电子邮件经过验证
