| Proportional closed-loop feedback control of flow separation JT Pinier, JM Ausseur, MN Glauser, H Higuchi AIAA journal 45 (1), 181, 2007 | 137 | 2007 |
| Feedback control of separated flows MN Glauser, H Higuchi, J Ausseur, J Pinier, H Carlson AIAA paper 2521, 2004, 2004 | 73 | 2004 |
| Experimental Development of a Reduced Order Model for Flow Sepapration Control J Ausseur, J Pinier, M Glauser, H Higuchi, H Carlson 44th AIAA Aerospace Sciences Meeting and Exhibit, 1251, 2006 | 32 | 2006 |
| Two-point correlations of the near and far-field pressure in a transonic jet JW Hall, J Pinier, A Hall, M Glauser ASME Paper FEDSM2006-98458, 2006 | 31 | 2006 |
| Towards closed-loop feedback control of the flow over NACA-4412 airfoil JM Ausseur, JT Pinier AIAA Paper 343, 2005 | 23 | 2005 |
| Aerodynamic Analyses and Database Development for Ares I Vehicle First Stage Separation BN Pamadi, J Pei, JT Pinier, GH Klopfer, SD Holland, PF Covell & Proceedings 저널· 프로시딩즈| 기술보고서| 해외연구초록| Reference DB| 공학 …, 0 | 23* | |
| Ares I Aerodynamic Testing at the Boeing Polysonic Wind Tunnel JT Pinier, JN Charles, JL Hanke, WG Tomek & Proceedings 저널· 프로시딩즈| 기술보고서| 해외연구초록| Reference DB| 공학 …, 0 | 21* | |
| Cross-spectral analysis of the pressure in a Mach 0.85 turbulent jet JW Hall, AM Hall, JT Pinier, MN Glauser AIAA journal 47 (1), 54-59, 2009 | 18 | 2009 |
| Advances in the Characterization of NASAā€™ s Space Launch System Aerodynamic Environments JT Pinier, A Herron, RJ Gomez AIAA Aviation 2019 Forum, 3397, 2019 | 17 | 2019 |
| Flow separation control using a convection based POD approach J Ausseur, J Pinier, M Glauser 3 rd AIAA Flow Control Conference; San Francisco, CA, 2006 | 16 | 2006 |
| Ascent Aerodynamic Force and Moment Database Development for the Space Launch System PR Shea, JT Pinier, H Houlden, A Favaregh, MJ Hemsch, DJ Dalle, ... AIAA Aviation 2019 Forum, 3298, 2019 | 14 | 2019 |
| Sonic boom pressure signature uncertainty calculation and propagation to ground noise E Walker, JT Pinier, T West, K Bretl 53rd AIAA Aerospace Sciences Meeting, 1251, 2015 | 14 | 2015 |
| Space Launch System Liftoff and Transition Aerodynamic Characterization in the NASA Langley 14x22'Subsonic Wind Tunnel JT Pinier, GE Erickson, J Paulson, WG Tomek, D Bennett, JA Blevins 53rd AIAA Aerospace Sciences Meeting, 0775, 2015 | 14 | 2015 |
| Controller Development for Closed-Loop Feedback Control of Flows JM Ausseur, JT Pinier, MN Glauser, H Higuchi, H Carlson 35 th AIAA Fluid Dynamics Conference and Exhibit; Toronto, Ontario, 1-11, 2005 | 14 | 2005 |
| Reduced-order model for NASA space launch system liftoff aerodynamics HA Carlson, R Verberg, JT Pinier, SE Krist 53rd AIAA Aerospace Sciences Meeting, 0777, 2015 | 13 | 2015 |
| Space launch system booster separation aerodynamic database development and uncertainty quantification DT Chan, DJ Dalle, SE Rogers, JT Pinier, FJ Wilcox, RJ Gomez 54th AIAA Aerospace Sciences Meeting, 0798, 2016 | 12 | 2016 |
| Space Launch System Ascent Static Aerodynamics Database Development JT Pinier, DW Bennett, GE Erickson, NM Favaregh, HP Houlden, ... 52nd Aerospace Sciences Meeting, 1254, 2014 | 11 | 2014 |
| Low-dimensional techniques for active control of high-speed jet aeroacoustics J Pinier Syracuse University, 2007 | 11 | 2007 |
| Identifying the most energetic modes of the pressure near-field region of a Mach 0.85 axisymmetric jet AM Hall, JT Pinier, JW Hall, MN Glauser AIAA Paper 314, 2006, 2006 | 11 | 2006 |
| Space Launch System Booster Separation Aerodynamic Testing at the NASA Langley Unitary Plan Wind Tunnel F Wilcox, JT Pinier, DT Chan, WA Crosby 54th AIAA Aerospace Sciences Meeting, 0796, 2016 | 10 | 2016 |
M GlauserProfessor of Mechanical and Aerospace Engineering, Syracuse UniversityVerified email at syr.edu
