Portfolio · 2026

ANISH
DHAR

Mechanical Engineer · Pune, India · Pharma · Motorsport · CFD

ABOUT

Mechanical engineer with a strong background in structural and thermal simulation and end-to-end product development — taking complex assemblies and novel joining systems from initial concept all the way to manufacturing release. Based in Pune, India.

At Glatt Systems, I took complete design ownership of a first-of-its-kind containment bin-washing solution for highly potent APIs — a structure over 9 metres tall, partially embedded in the ground, with specialised containment valves, washing bins from 600 to 2500 litres — and of the Glatt iEP lab-scale extruder spheronizer, guided through its full development cycle from mechanical CAD to manufacturing, functional testing, and exhibition. I delivered the full design packages and BOMs from scratch while coordinating procurement and manufacturing.

Alongside product work, I bring a digital mindset to engineering: from-scratch CFD solvers in Python. Engineering by instinct, verified by numbers.

Autodesk Inventor SolidWorks ANSYS FEA / CFD Python · PINN / SPH DVPR / DFMEA FDM / SLA AM Vault PDM

PROJECTS

Glatt iEP lab-scale extruder spheronizer
PROJECT 02 · GLATT IEP
Design OwnershipSolo ProjectFirst-of-Kind
iEP — Lab-Scale Extruder Spheronizer

Design ownership of the Glatt iEP, a first-of-its-kind vertical integrated lab-scale extruder spheronizer, guided through its complete development cycle — mechanical CAD, manufacturing, functional testing, and presentation at industry exhibitions. The tool-less, all-in-one design allows rapid changeover between pharmaceutical formulations without disassembly.

Specification Gist
RoleDesign ownership, manufacturing mgmt., testing & process improvement (solo)
Batch size≤ 1 kg (lab-scale)
ChangeoverTool-less, fully integrated all-in-one package
DriveServo-motor driven
MaterialsVenlafaxine, tamsulosin, and other pharmaceutical actives
InnovationFirst-of-its-kind vertical integrated extruder spheronizer
Boltless flanged duct assembly on shop floor
PROJECT 03
Pressure SystemsNovel Joint Design
Boltless Twist-Lock Ducting Joinery

Designed a twist-lock joining mechanism for large-diameter process ducting at Glatt Systems, replacing legacy flanged plant joints. The design cuts assembly steps and field installation complexity versus bolted flanges. Prototype qualified at 2 bar in a single-connection acceptance test.

Specification Gist
Test pressure2 bar (single-connection qualification)
MaterialSS316 pharma-grade
InnovationBoltless twist-lock joint; flanged-joint elimination
3-story all-steel vertical granulation structure
PROJECT 04
Structural DesignMulti-storyPharma OEM
3-Story Vertical Granulation Line

Contributed structural design to a 3-story all-steel vertical granulation line for a global pharmaceutical OEM, built for pre-production validation. Part of a 4-member core team coordinating across mechanical, process, and controls sub-teams.

Specification Gist
Structure3-story all-steel; cross-team coordination
ClientGlobal pharmaceutical OEM
Team4-member core (mech + process + controls)
FDM-printed jet-impingement manifold on e-BAJA car
PROJECT 05 · VJTI RACING
Thermal DesignAdditive Mfg.SAE e-BAJA
AM Jet-Impingement Motor Controller Enclosure

Engineered a jet-impingement cooling enclosure for the motor controller of VJTI Racing's e-BAJA entry using SLA and FDM additive manufacturing. Designed low-loss manifold geometry to minimise static pressure drop across the forced-air distribution network, reducing auxiliary battery load.

Specification Gist
Mass500 g enclosure (SLA/FDM)
Target ΔT−25 °C vs. baseline air-cooled config
ResultAIR 1 Sales Presentation, AIR 5 Overall — SAE e-BAJA 2024
VJTI Racing EV car
PROJECT 06 · VJTI RACING
EV SystemsHV/LV DesignSAE e-BAJAISIE IKR
EV Powertrain & Electrical Systems — SAE e-BAJA & ISIE IKR 2023

Led low- and high-voltage electrical system design for VJTI Racing across the SAE e-BAJA/ATVC and ISIE IKR 2023 EV entries. Implemented a multi-layer startup interlock sequence for HV safety. Recognised with Best Accelerating Vehicle, Best Business Proposal, and AIR 5 EV category.

Specification Gist
ScopeLV + HV system design lead
SafetyMulti-layer startup interlock sequence
AwardsBest Accelerating Vehicle, Best Business Proposal, AIR 5 EV
Clear-resin printed prototype of the converging-diverging nozzle, used for geometry validation
PROJECT 07
PropulsionPersonal Project
IPA–Air Rocket Engine Nozzle

Designed a converging-diverging nozzle for 300 N sea-level thrust using isopropyl alcohol-air propellant. Validated the internal flow geometry with a clear-resin printed prototype before machining the final nozzle in mild steel on a Jyoti VMC850, handling the fixturing design and toolpath programming.

Specification Gist
Design thrust300 N sea-level
PropellantIsopropyl alcohol — air
GeometryConverging-diverging (De Laval)
PrototypingResin-printed article for geometry check; final part CNC-machined mild steel
Post-testFailure analysis using DFMEA concepts
35T Electric Arc Furnace cooling circuit
PROJECT 08 · INTERNSHIP
Thermal AuditHeavy IndustryEAF
35T Electric Arc Furnace — Cooling Circuit Audit

Surveyed the water-cooling circuit of a 35T Electric Arc Furnace and continuous casting line at Saarloha Advanced Materials, using plant instrumentation data to identify thermal loss pathways caused by slag deposition on the cooling panels. Delivered a structured improvement report proposing design modifications to reduce parasitic heat losses, aligning with the site's green manufacturing targets.

Specification Gist
Equipment35T EAF + continuous casting line
FocusThermal loss pathways from slag deposition
MethodPlant instrumentation data analysis
OutputImprovement report; green manufacturing alignment

RESUME

Resume.pdf — Mechanical Engineer ↓ Download PDF
Glatt Systems
Engineering Trainee — New Product Development
Jun 2025 — Present · Pune, IN
  • Designed a boltless SS316 twist-lock ducting joint to eliminate legacy flanged connections on large-diameter process ducting; qualified the prototype at 2 bar in a single-connection acceptance test.
  • Complete design ownership of a first-of-its-kind containment bin-washing solution for highly potent APIs — 9+ m tall, partially ground-embedded, washing 600–2500 L bins; delivered full design package and BOMs from scratch.
  • Design ownership of a new lab-scale extruder spheronizer through its complete development cycle — mechanical CAD, manufacturing, functional testing, and presentation at industry exhibitions.
  • Designed and analysed a dedicated high-load test structure for trial and validation work, sizing members and joints against loading cases with structural FEA.
  • Built CAD automation and design tooling for the design group — iLogic mass-comparison tools, a parametric stair generator, and a BOM integrity checker validating assembly structure ahead of drawing release.
  • Managed 60+ Change Requests and Change Orders across assemblies of 200+ parts, with revision-controlled releases through Vault PDM, maintaining GD&T to ASME Y14.5 and tolerance stack-up calculations.
  • Incorporated shop-floor feedback to improve manufacturing processes across machining, sheet metal, and joining, with clear engineering calculations and tolerance stack-up documentation.
  • Contributed structural design to a 3-story all-steel vertical granulation line, collaborating across mechanical and process sub-teams through pre-production validation.
Saarloha Advanced Materials
Engineering Intern — Thermals
Jun 2024 — Aug 2024 · Pune, IN
  • Surveyed the water-cooling circuit of a 35T EAF and continuous casting line; identified thermal loss pathways from slag deposition using plant instrumentation data.
  • Delivered a structured improvement report proposing design modifications to reduce parasitic heat losses, aligning with the site's green manufacturing targets.
VJTI Racing
Thermal Systems & Electronics
Jan 2022 — Mar 2024 · Mumbai, IN
  • Jet-impingement cooling enclosure for motor controller (SLA/FDM AM); 500 g; target −25 °C vs. baseline air-cooled config.
  • Low-loss manifold geometry minimising static pressure drop, reducing auxiliary battery load.
  • AIR 1 Sales Presentation, AIR 5 Overall — SAE e-BAJA 2024.
  • LV + HV system design lead, ISIE IKR 2023; multi-layer startup interlock — Best Accelerating Vehicle, Best Business Proposal, AIR 5 EV.
VJTI Mumbai
B.Tech — Mechanical Engineering · Dec 2021 – May 2025
7.67 CGPA
City International School
HSC — CBSE · Jul 2021
88.2%
The Bishop's School
SSC — ICSE · May 2019
96.2%
Applied Computational Fluid Dynamics
Siemens · 2026
Cleanroom Fundamentals & Semiconductor Technologies
University at Buffalo · 2026
SOLIDWORKS: Design Study and Optimization
LinkedIn Learning · 2023
CAD / PDM
Autodesk Inventor
SolidWorks
Vault PDM
Simulation & AI
ANSYS Mechanical
ANSYS Fluent
MATLAB / Simulink
Python · PINN / SPH
Standards & Methods
DVPR / DFMEA
Tolerance Stack-up
BOM / Change Mgmt
GD&T (ASME Y14)
Manufacturing
Sheet Metal / Joining
FDM / SLA AM
Machining / Fixturing

COMPUTATIONAL WORK

Supersonic Flows in Sod Shock Tube
PythonEuler EquationsHyperbolic PDE

Numerical solution of the 1D Euler equations for the classical Sod shock tube problem. Implements Lax and MacCormack finite-difference schemes and benchmarks their accuracy and stability across varying grid subdivisions and CFL numbers. Captures the three characteristic wave structures: rarefaction fan, contact discontinuity, and shock front.

Governing eqs.
1D Euler (conserved form: ρ, ρu, E)
Schemes
Lax (1st-order) vs. MacCormack (2nd-order predictor-corrector)
Parameters swept
Grid subdivisions N, CFL number
Output
ρ, u, p profiles vs. exact Riemann solution
▶ MacCormack predictor step (conserved variables)
# Predictor: forward difference
U_pred[:, 1:-1] = U[:, 1:-1] - dt/dx * (F[:, 2:] - F[:, 1:-1])

# Corrector: backward difference on predicted fluxes
F_pred = compute_flux(U_pred)
U[:, 1:-1] = 0.5*(U[:, 1:-1] + U_pred[:, 1:-1]
             - dt/dx*(F_pred[:, 1:-1] - F_pred[:, :-2]))
Experiments in Computational Fluid Dynamics
PythonMATLABFDM

A collection of from-scratch numerical implementations spanning classical CFD problems: finite-difference schemes for the convection-diffusion equation, heat conduction, lid-driven cavity flow, and boundary layer analysis. Focuses on scheme accuracy, numerical diffusion, and grid convergence behaviour rather than commercial solvers.

Methods
FDM: explicit, implicit, Crank-Nicolson; upwind differencing
Problems
1D/2D heat eq., convection-diffusion, cavity flow (N-S)
Validation
Benchmarked against analytical solutions and published data
Language
Python (NumPy, Matplotlib) + MATLAB
▶ Upwind scheme for 1D convection-diffusion
# CFL = u·dt/dx, Pe = u·dx/ν (cell Peclet number)
for n in range(nt):
    u_new[1:-1] = (u[1:-1]
        - CFL*(u[1:-1] - u[:-2])         # upwind convection
        + (dt*nu/dx**2)*(u[2:] - 2*u[1:-1] + u[:-2])) # diffusion
    u = u_new.copy()
CFD 03 · CAPSTONE, VJTI
Numerical Investigation of Lattice-Based Cooling Structures
ANSYS FluentMesh ConvergenceHeat Transfer

Developed and meshed lattice unit-cell geometries in ANSYS Fluent, conducting mesh convergence studies to understand convective heat transfer enhancements and pressure-drop trade-offs across various candidate topologies.

Solver
ANSYS Fluent (conjugate heat transfer)
Geometry
Lattice unit cells, multiple candidate topologies
Method
Mesh convergence studies
Output
Heat transfer enhancement vs. pressure-drop trade-offs
FEA 04 · HONOURS, VJTI
Compressive Behavior of Vertically Graded Lattice Structures
ANSYS MechanicalLatticesEnergy Absorption

Modeled graded-density lattice structures under uniaxial compression using ANSYS Mechanical, extracting load-displacement curves via structural FEA to quantify their energy absorption.

Solver
ANSYS Mechanical (structural FEA)
Loading
Uniaxial compression
Geometry
Vertically graded-density lattices
Output
Load-displacement curves; energy absorption quantification