| Review of combustion stabilization for hypersonic airbreathing propulsion Q Liu, D Baccarella, T Lee Progress in Aerospace Sciences 119, 100636, 2020 | 198 | 2020 |
| Cavity flameholding in an optical axisymmetric scramjet in Mach 4.5 flows Q Liu, D Baccarella, W Landsberg, A Veeraragavan, T Lee Proceedings of the combustion institute 37 (3), 3733-3740, 2019 | 100 | 2019 |
| Unstart phenomena induced by mass addition and heat release in a model scramjet S Im, D Baccarella, B McGann, Q Liu, L Wermer, H Do Journal of Fluid Mechanics 797, 604-629, 2016 | 91 | 2016 |
| Ethylene flame dynamics and inlet unstart in a model scramjet Q Liu, A Passaro, D Baccarella, H Do Journal of Propulsion and Power 30 (6), 1577-1585, 2014 | 60 | 2014 |
| Cavity-enhanced combustion stability in an axisymmetric scramjet model Q Liu, D Baccarella, B McGann, T Lee AIAA journal 57 (9), 3898-3909, 2019 | 59 | 2019 |
| Development and testing of the ACT-1 experimental facility for hypersonic combustion research D Baccarella, Q Liu, A Passaro, T Lee, H Do Measurement Science and Technology 27 (4), 045902, 2016 | 56 | 2016 |
| Isolator-combustor interactions in a circular model scramjet with thermal and non-thermal choking-induced unstart D Baccarella, Q Liu, B McGann, G Lee, T Lee Journal of Fluid Mechanics 917, A38, 2021 | 53 | 2021 |
| Dual-mode operation and transition in axisymmetric scramjets Q Liu, D Baccarella, B McGann, T Lee AIAA journal 57 (11), 4764-4777, 2019 | 53 | 2019 |
| The supersonic combustion facility ACT-2 D Baccarella, Q Liu, T Lee, SD Hammack, H Do 55th AIAA Aerospace Sciences Meeting, 0103, 2017 | 50 | 2017 |
| A reduced order model for preliminary design and performance prediction of tapered inducers: comparison with numerical simulations L d'Agostino, L Torre, A Pasini, D Baccarella, A Cervone, A Milani 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 5119, 2008 | 49 | 2008 |
| Combustion induced choking and unstart initiation in a circular constant-area supersonic flow D Baccarella, Q Liu, BJ McGann, T Lee AIAA journal 57 (12), 5365-5376, 2019 | 37 | 2019 |
| Influences of inlet geometry modification on scramjet flow and combustion dynamics Q Liu, D Baccarella, T Lee, S Hammack, CD Carter, H Do Journal of Propulsion and Power 33 (5), 1179-1186, 2017 | 34 | 2017 |
| Laser-induced plasma ignition experiments in a direct-connect supersonic combustor at Mach 3 D Baccarella, GS Lee, Q Liu, GS Elliott, JB Freund, T Lee Journal of Propulsion and Power 36 (5), 732-743, 2020 | 28 | 2020 |
| Influences of freestream turbulence on flame dynamics in a supersonic combustor Q Liu, D Baccarella, S Hammack, T Lee, CD Carter, H Do AIAA journal 55 (3), 913-918, 2017 | 27 | 2017 |
| Material-aero-thermal interaction computations in the ATLLAS European programme M Bouchez, F Cheuret, P Grenard, JA Redford, ND Sandham, GT Roberts, ... 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 4670, 2008 | 27 | 2008 |
| Inlet unstart of an ethylene-fueled model scramjet with a Mach 4.5 freestream flow A Do, H: Passaro, D Baccarella | 22* | 2012 |
| Experimental investigation of single jet and dual jet injection in a supersonic combustor Q Liu, D Baccarella, B McGann, T Lee, H Do 2018 AIAA Aerospace Sciences Meeting, 1363, 2018 | 21 | 2018 |
| Multi-Level Coupled Simulations of Cooled Structures in the ATLLAS European Program M Bouchez, E Dufour, F Cheuret, J Steelant, P Grenard, L Benezech, ... 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and …, 2009 | 19 | 2009 |
| Ethylene flame dynamics in an arc-heated hypersonic wind tunnel H Do, A Passaro, Q Liu, T Lee, D Baccarella | 16 | 2013 |
| Experimental investigations on the magneto-hydro-dynamic interaction around a blunt body in a hypersonic unseeded air flow A Cristofolini, CA Borghi, G Neretti, A Schettino, E Trifoni, F Battista, ... Journal of Applied Physics 112 (9), 2012 | 15 | 2012 |
Qili LiuPurdue University; University of Illinois at Urbana-ChampaignEmail verificata su purdue.edu