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person:(Kumar, S.)

    Boundary layer Blockage, Venturi Effect and Cavitation Causing Aerodynamic Choking and Shock Waves in Human Artery Leading to Hemorrhage and Massive Heart Attack – A New Perspective

    Sanal Kumar, VR / Sankar, Vigneshwaran / Chandrasekaran, Nichith et al. | AIAA | 2018

    A Hybrid Approach to Model the Temperature Effect in Tire Forces and Moments

    Pandey, Ashok Kumar / S, Bibin | SAE Technical Papers | 2017

    Large eddy simulations of supersonic rectangular jets from sinuous exhaust system

    Brès, Guillaume A. / Bose, Sanjeeb / Ham, Frank et al. | AIAA | 2017

    Optimized Fuzzy Logic-Based Adaptive Cruise Control Vehicle for Urban and Highway Driving Patterns

    Paul Sathiyan, S. / Suresh Kumar, S. / Immanuel Selvakumar, A. | Springer Verlag | 2016

    Effect of Reynolds Number on 3-D Shock Wave Boundary Layer Interactions

    Baldwin, Andrew K. / Arora, Nishul / Kumar, Rajan et al. | AIAA | 2016

    CFD based Prediction of Spin Power Loss of Automotive Differential System

    Shome, Biswadip / Renjith, S / Srinivasa, Vinod Kumar | SAE Technical Papers | 2015

    A new methodology for determining accident and injury contributing factors, and its application to road accidents on the Mumbai-Pune Expressway

    Free access
    Patel, M. / Kumar, S. / Balakumar, S. et al. | ELBA - Federal Highway Research Institute (BASt) | 2015

    Development of Dual Fuel (Diesel-CNG) Engine for SUV Application in India

    Kulkarni, Ajit Vinayak / Sinha, Kausik / Kavathekar, Kishor Kumar et al. | SAE Technical Papers | 2015

    Conjugate Heat Transfer from an Impingement and Film-Cooled Flat Plate

    Panda, Rajesh Kumar / Prasad, B. V. S. S. S. | AIAA | 2014

    Reynolds Number Effects on the Performance of Small-Scale Propellers

    Deters, Robert W. / Ananda Krishnan, Gavin Kumar / Selig, Michael S. | AIAA | 2014

    Propeller-Induced Flow Effects on Wings of Varying Aspect Ratio at Low Reynolds Numbers

    Ananda Krishnan, Gavin Kumar / Deters, Robert W. / Selig, Michael S. | AIAA | 2014

    DHAKSHA,THE UNMANNED AIRCRAFT SYSTEM IN ITS NEW AVATAR-AUTOMATED AERIAL INSPECTION OF INDIA'S TALLEST TOWER

    Free access
    K. S. Kumar / A. Mohamed Rasheed / R. Krishna Kumar et al. | DOAJ | 2013

    Propeller Induced Flow Effects on Wings at Low Reynolds Numbers

    Ananda Krishnan, Gavin Kumar / Deters, Robert W. / Selig, Michael S. | AIAA | 2013

    Effect of Heat Pipe Figure of Merit on an Evaporating Thin Film

    Jasvanth, V. S. / Ambirajan, Amrit / Kumar, Dinesh et al. | AIAA | 2013

    Effect of Geometry on Droplet Formation in a Microfluidic Flow-Focusing Device

    Matharoo, Harpreet S. / Makkar, Devavret / Gupta, Amit et al. | AIAA | 2013

    Internal Wall-Jet Film Cooling with Straight Cylindrical Holes

    Shine, S. R. / Kumar, S. Sunil / Suresh, B. N. | AIAA | 2012

    Convective Heat Transfer Characterization of Aviation Turbine Fuel-Metal Oxide Nanofluids

    Sonawane, Sandipkumar / Bhandarkar, Upendra / Puranik, Bhalchandra et al. | AIAA | 2012

    Theoretical Studies of Hard Filling in Loop Heat Pipes

    Adoni, Abhijit A. / Ambirajan, Amrit / Jasvanth, V. S. et al. | AIAA | 2010

    Effects of Mass of Charge on Loop Heat Pipe Operational Characteristics

    Adoni, Abhijit A. / Ambirajan, Amrit / Jasvanth, V. S. et al. | AIAA | 2009

    Thermal Contact Conductance of Molybdenum-Sulphide-Coated Joints at Low Temperature

    K Ramamurthi / S Kumar / P Abilash | AIAA | 2007

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