UAV Integration • CAD + CFD

Aerospace engineer building mission-ready UAV systems

I design, integrate, prototype, and optimize unmanned systems across carbon-fiber drones, heavy-lift platforms, aerodynamic concepts, and simulation-backed flight hardware.

150+km/h UAV platform speed
16 kgHeavy-lift payload class
400+Students reached through workshops

Selected projects

UAV structures, aerodynamic experiments, rocket analysis, and conceptual aircraft design — from sketch through CAD, CFD, and flying hardware.

Quadcopter carbon-fiber frame — 1 of 2
Fusion 360Carbon frame

Quadcopter carbon-fiber frame

Calculated, designed, and detailed a high-performance FPV quad frame in Fusion 360 with weight reduction in mind. Used GF1045 Propeller along with 10mm thickness for the drone arm.

Glider development study — 1 of 2
Fusion 360Glider

Glider development study

Fuselage–wing–tail integration showing aerodynamic proportions, stability thinking, and CAD surfacing discipline.

Delta-wing UAV concept — 1 of 2
Fusion 360Delta wing

Delta-wing UAV concept

Aggressive delta planform UAV concept exploring sweep, taper, and control surface placement for high-speed missions, also simulated for structural deformation.

Custom UAV airframe — 1 of 1
Fusion 360Airframe

Custom UAV airframe

UAV airframe with 2120mm Wingspan. designed based on the calculations, MTOW assumed of 3.5kg (including 1kg payload), Used SD7067 airfoil for balanced lift and stability.

Propeller design in Siemens NX — 1 of 2
Siemens NXPropeller

Propeller design in Siemens NX

Surface-focused propeller geometry with blade twist, chord taper, and pitch refinement for thrust-targeted builds.

Wingtip configuration comparison — 1 of 2
XFLR5Aerodynamics

Wingtip configuration comparison

Baseline, bent, and split-scimitar wingtip concepts compared with aerodynamic plots in XFLR5. along with the wing designs for each with Sd7067 airfoil.

OpenFOAM airfoil CFD — 1 of 1
OpenFOAMCFD

OpenFOAM airfoil CFD

CFD-led iteration on a custom airfoil using OpenFOAM (WSL) — pressure, velocity, and stall behavior comparisons.

Rocket configuration & stability — 1 of 2
OpenRocketStability

Rocket configuration & stability

Simulation-backed rocketry work showing CG/CP relationships, flight configuration logic, and measurable outputs.

Professional summary

Aerospace engineer focused on UAV design, systems integration, rapid prototyping, and engineering presentation.

Engineering experience shaped around design exploration, UAV development, and practical aerospace problem solving — concept generation, CAD modeling, geometry refinement, and analysis-supported studies that reflect a strong interest in aircraft and drone design.

My profile is strongest where design intent, systems integration, and engineering practicality meet.

Design focusUAV integration, calculations, mission systems, CAD, PFMEA, DFMEA, GD&T, conceptual design.
ModelingFusion 360, Siemens NX, FreeCAD concept geometry
AnalysisAnsys Fluent, XFLR5, OpenRocket, OpenFOAM (WSL)
SoftwareMission Planner, Betaflight, INAV, ArduPilot

High glide ratio- Hand thrown Glider.

Hand-thrown glider designed in Fusion 360 with a glide ratio of approximately 11. Drag to orbit, scroll to zoom.

Engineering toolchain

Aware of These software workflows, I am a Quick Learner and would continue to learn more.

FUSION 360

Airframe concepts, quad frames, gliders, wing structures, manufacturable assemblies, and visual renders.

Siemens NX

Surface-focused geometry including propeller modeling and advanced part development.

CFD / ANSYS

Aerodynamic reasoning, performance refinement, and evidence-backed iteration on custom geometries.

XFLR5 / OPENROCKET

Concept screening, stability analysis, and early-stage validation for fixed-wing and rocket systems.

Integration stack

ArduPilot, Betaflight, INAV, ESP32 flight controllers, payload integration, and field deployment.

Experience

Engineering outcomes centered on performance, payload, integration, and deployment — across three labs in two years.

Turing

Freelance Aerospace Design EngineerMay 2026 – Present
  • Partnering with Turing on freelance aerospace design work — CAD modeling, geometry refinement, and design reviews delivered remotely.
  • Translating concept briefs into manufacturable airframe and component geometry across Fusion 360 and Siemens NX and freeCAD
  • Iterating on aerodynamic surfaces and structural layouts with quick-turn revisions tailored to each client's mission requirements. Worked on Xfoil, Xflr5 for the demonstration and simulations based on the requirements given as confidential problem statements.

Sentry Labs

Founding Aerospace EngineerSep 2025 – Present
  • Trained 400+ students and military personnel on drone fundamentals; guest-lectured at IIT Bombay and IIT Delhi.
  • Designed and commercialized an EPP-foam UAV; shipped engineering projects generating ₹300K–400K within 4 months.
  • Built ESP32-based drone and plane with in-house flight controller, BMI270 + BMP581 sensors, custom firmware.
  • Optimized custom UAV structures in Fusion 360 and Siemens NX for weight, structural integrity, and manufacturability.

Kalam Labs, Lucknow

Aerospace EngineerMar 2025 – Aug 2025
  • Engineered heavy-lift UAV systems including a 16 kg payload platform with optical-fiber integration.
  • Developed coaxial quadcopter drones (5 kg payload) with autonomous waypoint navigation.
  • Explored twin-fuselage, VTOL, tail-sitter, and box-wing aircraft for specialized missions.
  • Worked on a stratospheric kamikaze UAV with autonomous waypoint navigation, speeds up to 900 km/h.

Binford Research Labs Pvt. Ltd.

Aerospace Integration and Design EngineerJan 2024 – Feb 2025
  • Spearheaded high-speed UAVs reaching 150+ km/h with 20–25 min endurance and 2 kg payloads; tuned via ArduPilot and Betaflight.
  • Designed and fabricated custom carbon-fiber drone frames in Fusion 360 — 20% weight reduction with structural integrity preserved.
  • Deployed AI-enabled drone end-to-end: YOLOv5 detection, 2-axis gimbal tracking to 100 m, live GCS video.
  • Integrated heavy-lift systems (10–16 kg) including EO/IR cameras and comms relays for extended surveillance.

Profile

Systems-oriented aerospace engineer working from concept and CAD through assembly, tuning, and validation.

Aerospace engineer focused on high-performance UAV design, systems integration, and rapid prototyping. I'm strongest where CAD, integration, and practical deployment meet.

Trained 400+ students and military personnel on drone fundamentals; guest-lectured at IIT Bombay and IIT Delhi.

EducationB.E. Aerospace Engineering, Chandigarh University
FocusCAD design, UAV integration, aerodynamics, embedded prototyping
MethodsRapid prototyping, simulation-led design, iterative testing
IndustriesDefense UAVs, advanced prototyping, aerospace R&D
Available for design and integration roles

Let the work speak first, then the resume.

I'm open to UAV integration and design engineer positions where hands-on engineering is valued.

Emailaman.kumar.myr@gmail.com
Phone+91 8770257701
Role fitUAV Integration Engineer / Design Engineer
LocationIndia