Experimental Studies on the effect of Leading edge Tubercles on Laminar Separation Bubble N Karthikeyan, S Sudhakar, P Suriyanarayanan AIAA SciTech 2014 7, 9, 2014 | 42* | 2014 |
Experimental studies on a rudimentary four-wheel landing gear L Venkatakrishnan, N Karthikeyan, K Mejia AIAA journal 50 (11), 2435-2447, 2012 | 36 | 2012 |
Influence of leading edge tubercles on aerodynamic characteristics of a high aspect-ratio UAV S Sudhakar, N Karthikeyan, L Venkatakrishnan Aerospace Science and Technology 69, 281-289, 2017 | 33 | 2017 |
Experimental studies on the effect of leading-edge tubercles on laminar separation bubble S Sudhakar, N Karthikeyan, P Suriyanarayanan AIAA Journal 57 (12), 5197-5207, 2019 | 21 | 2019 |
Effect of spike truncation on the acoustic behavior of annular aerospike nozzles N Karthikeyan, A Kumar, SB Verma, L Venkatakrishnan AIAA journal 51 (9), 2168-2182, 2013 | 21 | 2013 |
Acoustic characterization of jet interaction with launch structures during lift-off N Karthikeyan, L Venkatakrishnan Journal of Spacecraft and Rockets 54 (2), 356-367, 2017 | 20 | 2017 |
Experimental investigation of the acoustics of an annular aerospike nozzle flow N Karthikeyan, SB Verma, L Venkatakrishnan 15th AIAA/CEAS Aeroacoustics Conference (30th AIAA Aeroacoustics Conference …, 2009 | 14 | 2009 |
Application of photogrammetry to surface flow visualization N Karthikeyan, L Venkatakrishnan Experiments in fluids 50, 689-700, 2011 | 9 | 2011 |
An experimental investigation into the effect of nozzle spacing in supersonic twin jets Y Mehta, K Natarajan, J Gustavsson, R Kumar AIAA Scitech 2021 Forum, 1293, 2021 | 7 | 2021 |
Prediction of launch vehicle noise during lift-off using a modified Eldred's method SA Kumar, N Karthikeyan The 14th Asian Congress of Fluid Mechanics, 2013 | 7 | 2013 |
Effect of nozzle spacing on flow and acoustics characteristics of supersonic twin jets impinging on an inclined surface K Natarajan, Y Mehta, J Gustavsson, R Kumar AIAA AVIATION 2021 FORUM, 2220, 2021 | 6 | 2021 |
Density field measurements of a micro–explosion using BOS P Suriyanarayanan, N Karthikeyan, L Venkatakrishnan, O Samuelraj, ... 28th International Symposium on Shock Waves: Vol 2, 705-710, 2012 | 6 | 2012 |
Shock-wave/boundary-layer interactions on an axisymmetric body at Mach 2 F Mason, K Natarajan, R Kumar AIAA Journal 59 (11), 4530-4543, 2021 | 5 | 2021 |
Effect of Leading edge tubercles on flow field over NACA-4415 airfoil at low Reynolds number S Sudhakar, N Karthikeyan The 14th Asian Congress of Fluid Mechanics-14ACFM October, 15-19, 2013 | 5 | 2013 |
Flow Separation Control on a NACA-4415 Airfoil at Low Reynolds Number S Sudhakar, N Karthikeyan Proceedings of 16th Asian Congress of Fluid Mechanics, 323-334, 2021 | 4 | 2021 |
Flow Field and Acoustic Investigations of the Launch Vehicle Environment during Lift-off K Natarajan, L Venkatakrishnan 21st AIAA/CEAS Aeroacoustics Conference, 3121, 2015 | 3 | 2015 |
Correlation studies in the acoustic far-field of non-ideally expanded supersonic jets A Kumar, N Karthikeyan, L Venkatakrishnan AIAA Paper 2082, 2013, 2013 | 3 | 2013 |
Experimental investigations and evaluation of MAV planforms R Mukund, N Karthikeyan PD EA 921, 2009 | 3 | 2009 |
Application of Phase-Averaging Methods to Sweeping Supersonic Jets AK Subramanyam, K Natarajan, L Venkatakrishnan, R Woszidlo, ... AIAA Journal 60 (2), 699-711, 2022 | 2 | 2022 |
Investigation of the interaction between a steady jet and an impulsively started jet using Schlieren imaging K Natarajan, JN Murugan, S Sathiyavageeswaran AIAA Scitech 2020 Forum, 1803, 2020 | 2 | 2020 |