Centre of Excellence for Computational Mechanics Ramaiah Group 1 - - PowerPoint PPT Presentation

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Centre of Excellence for Computational Mechanics Ramaiah Group 1 - - PowerPoint PPT Presentation

Centre of Excellence for Computational Mechanics Ramaiah Group 1 Outline Structure of Centre of Excellence in Computational Mechanics Centre of Excellence Researchers Vision, Mission and Goals of Centre of Excellence Research


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1

Centre of Excellence for Computational Mechanics

Ramaiah Group

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Outline

  • Structure of Centre of Excellence in Computational

Mechanics

  • Centre of Excellence Researchers
  • Vision, Mission and Goals of Centre of Excellence
  • Research activities carried out
  • Research Areas of Interests to be Explored
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SLIDE 3

3 Structural Dynamics and Earthquake Engineering

  • Modal, Harmonic, Shock and Random

vibration analysis

  • Earthquake Geotechnical Engineering

Computational Fluid Dynamics

  • Low Reynolds number flows
  • External flows
  • Internal flows
  • Fluid-structure interaction
  • Multi-Disciplinary Analysis and

Optimisation

Computational Structural Mechanics

  • Structural Analysis and Optimisation
  • Composites
  • Damage Tolerant Design

Structure of Centre of Excellence in Computational Mechanics

Computational Mechanics

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4

CoE Researchers

  • Dr. Rahul M.

Cadambi Associate Professor, Dept. of Mechanical and Manufacturing Engg, RUAS B.E.,

  • M. Tech, Ph. D.

Composites Damage Tolerant Design and Polymer Nanocomposites

  • Prof. H . K.

Narahari Professor, Dept. of Aerospace Engg, RUAS B.Sc., D.M.I.T [Aero], M.E., Ph.D. Aircraft Design, Aerodynamic Shape Optimization and MDO

  • Dr. M.

Sivapragasam Associate Professor, Dept. of Aerospace Engg, RUAS M.Sc. (Engg),

  • Ph. D.

Low Reynolds Number Aerodynamics, Aerodynamic Shape Optimization

  • Dr. Anitha

Kumari Associate Professor, Dept. of Civil Engg, RUAS B.Tech, M.S. (Res), Ph. D. Discrete Element Modelling, Soil Liquefaction

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CoE Researchers (Continued)

  • Prof. Dinesh P.

Professor, Dept. of Mechanical Engg, RIT B.E., M.E., Ph.D. Finite Element Method and Fracture Mechanics

  • Dr. Dinesh P. A.

Associate Professor, Dept. of Mathematics, RIT

  • M. Sc., M. Sc.

(IT), M. Phil.,

  • Ph. D.

Heat and Mass Transfer, Fluid Flows, Computational Fluid Dynamics, Bio – Mechanics, Statistical Analysis and Modeling

  • Mr. Basavana

Gowda G. M. Assistant Professor, Dept. of Civil Engg, RIT B.E, M. Tech., (Ph.D.) Earthquake Engineering, Soil Dynamics, Structural Dynamics

  • Mr. Parikshith N.

Technical Manager, Technocentre, RUAS B.E., M.Sc. (Engg) CFD, FSI, Heat Transfer and Composite Structure Simulation

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CoE Researchers (Continued)

  • Dr. B. Ramaswamy

Karthikeyan Associate Professor,

  • Dept. of Electronics

and Communication Engg, RUAS

  • B. E., M.Sc.

(Engg.), Ph. D. Computational Electro- Magnetics, DSP Algorithms, Communication Engineering

  • Mr. Varun D.

Assistant Professor,

  • Dept. of Electronics

and Communication Engg, RUAS

  • B. E., M.Sc.

(Engg.) Computational Electro- Magnetics, Modelling of RF Front-End and Communication Engineering

  • Mr. Nagaraju T. R.

Project Engineer, Technocentre, RUAS B.E., M. Tech Structural, Implicit and Explicit Dynamic Simulations

  • Mr. Siddarth Akki

Project Engineer, Technocentre, RUAS

  • B. E., M. Tech

CFD, Heat Transfer and Structural Simulation

  • Mr. Sheel Kumar

Srivastava Valdel Advanced Technologies Ltd., Bengaluru B.Tech., M. Tech. FEA, Structural Analysis of Composites and Metals

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Vision and Mission of CoE

Vision

  • To build a pro-active multi-disciplinary computational mechanics

research group involving academicians, researchers and students to solve contemporary research problems of interest to academia and industry

Mission

  • To apply computational mechanics framework to solve contemporary

research problems in structural mechanics and fluid mechanics

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Envisaged Goals of CoE

  • To

teach and explore

  • utreach

in the field

  • f

Computational Fluid Dynamics and Computational Structural Mechanics

  • To establish synergy between academia and industry for

pursuing high end applied research

  • To transfer technologies developed for commercialization

and entrepreneurship

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Composites – Structures, Damage Tolerant Design

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Failure of Composites – Curing Defects in T Joints

Modelling Approach Pull-Out Results Parametric Studies for Lay-up Optimisation

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Microstructural Damage of Single Fibre Composites – Longitudinal Loading

Modelling Approach A B C Simulation Results

Experimental Results1

1 Mat. Sci. Eng. A, 2008

Simulation Results

Comparison of Microstructural Damage of Experimental and Simulation Observation

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Microstructural Damage of Single Fibre Composites – Transverse Shear Loading

Modelling Approach Simulation Results Simulation of Microstructural Damage A B C D E

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Machining damage – MD-CFRP Conventional Drilling

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Machining damage – MD-CFRP Conventional Drilling

Delamination study at Drill entry Experiment and Simulation Composites Drilling Process Parameters (a) Experiment and (b) Simulation (a) (b)

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15 Modal Shock Vibration Vibration Fatigue Buckling and Implosion Impact

Structural Analysis

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16 Double Display Unit Receiver Cabinet Single Display Unit Three Axis Tracker Mount APD P07 Unit Chiller Unit

Structural Analysis of Electronic Consoles

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Replacement of Metallic Battery Panel to Composite

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Finite Difference Modelling (Liquefaction Analysis)

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CFD Analysis

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Iteration ( Cl / Cd )max

10 20 30 40 50 60 3.6 3.7 3.8 3.9 4

V-5 V-15 V-25 V-35 V-50

x/c y/c

1 0.78 0.56 0.34 0.12

  • 0.1
  • 0.32
  • 0.54
  • 0.76
  • 0.98
  • 1.2

1.5 1 0.1 0.2 0.5

  • 0.2
  • 0.1

Optimization at Ultra-Low Reynolds Numbers

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21 Re = 50,000 α = 1˚, Cl = -0.0299

Aerodynamics of Low Reynolds Number Flows

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 (deg) CL

1 2 3 4 5 6 7 8 0.02 0.04 0.06 0.08 0.1 0.12 0.14 0.16 0.18 0.2 0.22 0.24

Re = 50,000 Re = 100,000 Re = 150,000

 (deg) CD

1 2 3 4 5 6 7 8 0.02 0.025 0.03 0.035 0.04 0.045 0.05

Re = 50,000 Re = 100,000 Re = 150,000

Propeller Slipstream Effects on MAV Wing

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23 Rao et al., SAROD 2018

Wing Optimization for Transonic Business Jet

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Supersonic Retropropulsion

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25 Internal Aerodynamics External Aerodynamics Engine Cooling BLDC Generator Electromagnetic and Thermal Analysis

CFD Analysis

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26 C Band Unit K Band Unit CNT-DIO Cards TRMM Unit

Thermal/Heat Transfer Analysis of Electronic Console

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Characteristics of Shock Vector Controlled Fluid Thrust Vectoring System for Jet Engine

Shock controlled fluidic thrust vectoring at -with

  • ut and with secondary fluidic injection

Sponsoring Agency: Aeronautics Research & Development Board (AR&DB)

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Prediction of Bird-hit Damage on Fan Blades in an Aircraft Engine

FE model of fan blade with disc and bird

Stress distribution in blade at without and with pre-stress condition

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Cooling Concepts Related to Gas Turbine Blades

Geometry of a turbine blade showing all cooling methods Comparison between present computation and published literature of thermal contours at different planes

Sponsoring Agency: Gas Turbine Research Establishment (GTRE), Bangalore under GATET

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30 30

Discrete Element Modelling (DEM)

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  • 60
  • 40
  • 20

20 40 60 2 4 6 8 10 12 14 Deviatoric stress (kPa) No of cycles

Confining pressure = 100kPa Frequency = 1Hz Amplitude of strain rate = 0.006

  • 60
  • 40
  • 20

20 40 60

  • 5
  • 4
  • 3
  • 2
  • 1

Deviatoric stress (kPa) Axial strain (%)

Confining pressure = 100kPa Frequency = 1Hz Amplitude of strain rate = 0.006

0.0 0.2 0.4 0.6 0.8 1.0 2 4 6 8 10 12 Pore pressure ratio No of cycles

Confining pressure = 100kPa Frequency = 1Hz Amplitude of strain rate = 0.006

  • 1
  • 0.5
0.5 1
  • 1
  • 0.8
  • 0.6
  • 0.4
  • 0.2
0.2 0.4 0.6 0.8 1
  • 1
  • 0.8
  • 0.6
  • 0.4
  • 0.2
0.2 0.4 0.6 0.8 1
  • 1
  • 0.5
0.5 1
  • 1
  • 0.5
0.5 1
  • 1
  • 0.8
  • 0.6
  • 0.4
  • 0.2
0.2 0.4 0.6 0.8 1
  • 1
  • 0.8
  • 0.6
  • 0.4
  • 0.2
0.2 0.4 0.6 0.8 1
  • 1
  • 0.5
0.5 1
  • 1
  • 0.5
0.5 1
  • 1
  • 0.5
0.5 1
  • 1
  • 0.5
0.5 1
  • 1
  • 0.5
0.5 1
  • 1
  • 0.5
0.5 1
  • 1
  • 0.5
0.5 1
  • 1
  • 0.5
0.5 1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1
  • 0.1
  • 0.05
0.05 0.1

Normal contact force histograms Spherical harmonic distribution of normal contact force Spherical harmonic distribution of tangential contact force

Discrete Element Modelling

Liquefaction behaviour

Isotropic Compression Extension Near to liquefaction

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Profile at the end of second failure due to landslide

Landslide: Slope Stability Underground Tunnels Rice Polishing Machine

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33 33

Computational Electro-Magnetics (CEM)

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~48 mm ~80 mm Vivaldi Array Vivaldi Array Beamsteering

Vivaldi Array

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RAS ARRAY PLACEMENT ON WING

Vivaldi Array Placement Studies

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Thermal Analysis of Three Phase Squirrel Cage Induction Motor for Computation of Minimum Temperature

Prediction of temperature under steady state condition for rated load Air flow vector plot Vector plot of Air flow over the fins Plane section of motor

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Simulation Studies on Time Domain Analysis of Magnetic Flux in Three Phase Squirrel Cage Induction Motor

Magnetic Flux Density in Stator, Rotor and Air-gap

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Computational Electromagnetic Simulations

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Research Areas of Interests to be Explored Computational Structural Mechanics

  • Continuous Damage Mechanics (CDM) of composite materials
  • Composites microstructural modeling of delamination and intra-

laminar crack for failure analysis

  • Multi-scale modeling and fracture simulation for energy absorption

in composites

Computational Fluid Dynamics

  • Modelling of separated flows
  • Modelling of hypersonic flows including ionization effects
  • Modelling of chemically reacting flows
  • Smoothed Particle Hydrodynamics (SPH) Simulations
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Research Areas of Interests to be Explored (Continued) Coupled flow (CFD-DEM) Structural Dynamics

  • Shake Table Studies on performance of structures and slopes

Computational Electro-Magnetics (CEM)

  • High frequency CEM
  • Avionics in hypersonic applications
  • CEM for magneto-hydrodynamics