| Dependence of minimum ignition energy on ignition parameters A Frendi, M Sibulkin Combustion science and technology 73 (1-3), 395-413, 1990 | 104 | 1990 |
| Flow past a backward-facing step: Comparison of PANS, DES and URANS results with experiments A Frendi, A Tosh, S Girimaji International Journal for Computational Methods in Engineering Science and …, 2006 | 81 | 2006 |
| Uncertainty quantification of turbulence model coefficients via Latin hypercube sampling method MC Dunn, B Shotorban, A Frendi | 64 | 2011 |
| Coupling between plate vibration and acoustic radiation A Frendi, L Maestrello, A Bayliss Journal of Sound and Vibration 177 (2), 207-226, 1994 | 64 | 1994 |
| Prediction of flammability limit of an unconfined premixed gas in the absence of gravity M Sibulkin, A Frendi Combustion and flame 82 (3-4), 334-345, 1990 | 58 | 1990 |
| Integrated aeropropulsive computational fluid dynamics methodology for the Hyper-X flight experiment CE Cockrell Jr, WC Engelund, RD Bittner, TN Jentink, AD Dilley, A Frendi Journal of spacecraft and rockets 38 (6), 836-843, 2001 | 54 | 2001 |
| Study of the ignition overpressure suppression technique by water addition F Canabal, A Frendi Journal of spacecraft and rockets 43 (4), 853-865, 2006 | 45 | 2006 |
| Combustion properties of pure and fire-retarded cellulose Y Chen, A Frendi, SS Tewari, M Sibulkin Combustion and Flame 84 (1-2), 121-140, 1991 | 39 | 1991 |
| Nonlinear vibration and radiation from a panel with transition to chaos L Maestrello, A Frendi, DE Brown AIAA journal 30 (11), 2632-2638, 1992 | 38 | 1992 |
| Implicit Thermochemical Nonequilibrium Flow Simulations on Unstructured Grids using GPUs G Nastac, A Walden, E Nielsen, A Frendi AIAA Scitech Forum, 2021 | 30 | 2021 |
| On the effect of acoustic coupling on random and harmonic plate vibrations A Frendi, J Robinson AIAA journal 31 (11), 1992-1997, 1993 | 30 | 1993 |
| Integrated aero-propulsive CFD methodology for the Hyper-X flight experiment C Cockrell, Jr, W Engelund, A Dilley, R Bittner, T Jentink, A Frendi 18th Applied Aerodynamics Conference, 4010, 2000 | 28 | 2000 |
| Coupling between a supersonic turbulent boundary layer and a flexible structure A Frendi AIAA journal 35 (1), 58-66, 1997 | 28 | 1997 |
| A Computational and experimental study of linear aerospike engine noise A Frendi, TE Nesman, TS Wang AIAA journal 39 (8), 1485-1492, 2001 | 24 | 2001 |
| An efficient model for coupling structural vibrations with acoustic radiation A Frendi, L Maestrello, L Ting Journal of sound and vibration 182 (5), 741-757, 1995 | 24 | 1995 |
| Experimental investigation of a bioinspired bluff-body effect on galloping piezoelectric energy-harvester performance F Ewere, G Wang, A Frendi Aiaa Journal 56 (3), 1284-1287, 2018 | 23 | 2018 |
| On the coupling between a supersonic boundary layer and a flexible surface A Frendi, L Maestrellot, A Baylisst AIAA journal 31 (4), 708-713, 1993 | 19 | 1993 |
| A jet engine noise measurement and prediction tool A Frendi, WD Dorland, T Maung, T Nesman, TS Wang The Journal of the Acoustical Society of America 112 (5), 2036-2042, 2002 | 18 | 2002 |
| Interaction of three-dimensional protuberances with a supersonic turbulent boundary layer PV Hahn, A Frendi AIAA journal 51 (7), 1657-1666, 2013 | 17 | 2013 |
| Supersonic Jet Impingement on a Flat Plate MR Brown, A Frendi 18th AIAA/CEAS Aeroacoustics conference, AIAA-2012-2261, 2012 | 16 | 2012 |
Alvin BaylissProfessor, Engineering Sciences and Applied Mathematics - Northwestern UniversityEmail được xác minh tại northwestern.edu
