| Aeroacoustics of twin supersonic jets: a review G Raman, P Panickar, K Chelliah International Journal of Aeroacoustics 11 (7-8), 957-984, 2012 | 46 | 2012 |
| Criteria for the existence of helical instabilities in subsonic impinging jets P Panickar, G Raman Physics of Fluids 19 (10), 2007 | 40 | 2007 |
| The effect of heat on turbulent mixing noise in supersonic jets W Baars, C Tinney, N Murray, B Jansen, P Panickar 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2011 | 31 | 2011 |
| Aeroacoustic features of coupled twin jets with spanwise oblique shock-cells P Panickar, K Srinivasan, G Raman Journal of sound and vibration 278 (1-2), 155-179, 2004 | 28 | 2004 |
| Aeroacoustics of a planar multistream supersonic nozzle with aft deck and sidewalls CE Tinney, P Panickar, P Vogel AIAA Journal 56 (10), 3926-3937, 2018 | 23 | 2018 |
| Study of coupled supersonic twin jets of complex geometry using higher-order spectral analysis K Srinivasan, P Panickar, G Raman, BH Kim, DR Williams Journal of sound and vibration 323 (3-5), 910-931, 2009 | 18 | 2009 |
| A laboratory framework for synchronous near/far-field acoustics and MHz PIV in high-temperature, shock-containing, jets N Murray, G Lyons, CE Tinney, B Donald, W Baars, B Thurow, H Haynes, ... Noise Control and Acoustics Division Conference 45325, 505-519, 2012 | 14 | 2012 |
| Localization of acoustic sources in shock-containing jet flows using phased array measurements P Panickar, N Sinha, N Murray 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and …, 2013 | 13 | 2013 |
| Acoustic source localization of rectangular jets using large eddy simulation with numerical phased arrays JP Erwin, P Panickar, P Vogel, N Sinha 52nd Aerospace Sciences Meeting, 0179, 2014 | 12 | 2014 |
| Stability of a hybrid mean velocity profile and its relevance to cavity resonance suppression S Sarpotdar, P Panickar, G Raman Physics of Fluids 22 (7), 2010 | 12 | 2010 |
| Understanding the mechanism of cavity resonance suppression using a cylindrical rod in crossflow P Panickar, G Raman 46th AIAA Aerospace Sciences Meeting and Exhibit, 54, 2008 | 12 | 2008 |
| Nonlinear interactions as precursors to mode jumps in resonant acoustics P Panickar, K Srinivasan, G Raman Physics of Fluids 17 (9), 2005 | 12 | 2005 |
| Using linear stability analysis as a tool to evaluate jet and cavity flow control situations P Panickar, G Raman International Journal of Flow Control 1 (1), 43-72, 2009 | 9 | 2009 |
| Study of supersonic twin jet coupling using higher order spectral analysis K Srinivasan, P Panicker, G Raman, BH Kim, D Williams 33rd AIAA Fluid Dynamics Conference and Exhibit, 3871, 2003 | 9 | 2003 |
| Proper-orthogonal-decomposition-based reduced-order models for characterizing ship airwake interactions CE Tinney, J Shipman, P Panickar AIAA Journal 58 (2), 633-646, 2020 | 8 | 2020 |
| Acoustic source indicators using LES in a fully expanded and heated supersonic jet R Fiévet, CE Tinney, N Murray, G Lyons, P Panickar 19th AIAA/CEAS Aeroacoustics Conference, 2193, 2013 | 7 | 2013 |
| New Vortex Generator Design for Nozzle Internal Modification. P Panickar, SD Sharma, S Sarpotdar, G Raman, W Butler International Journal of Aerospace Innovations 3 (4), 2011 | 7 | 2011 |
| Cavity tone suppression using a rod in cross flow: Investigation of shear layer stability mechanism S Sarpotdar, P Panickar, G Raman 47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and …, 2009 | 7 | 2009 |
| Laboratory-Scale Afterburning Supersonic Jet Noise Reduction Using Contoured Inserts NE Murray, CE Tinney, P Panickar 28th AIAA/CEAS Aeroacoustics Conference, 14-17, 2022 | 6 | 2022 |
| Mode switching and linear stability analysis of resonant acoustic flows P Panickar Illinois Institute of Technology, 2008 | 5 | 2008 |
