Summary
Overview
Work History
Education
Skills
Timeline
Generic

Haripriya K

Bengaluru

Summary

Organized and dependable candidate with 2 and half years of experience in aerostructural load analysis of fighter aircraft along with topology optimization of structure using adaptable algorithms and also skilled at automating workflow for lesser complexity.

Overview

3
3
Languages
2027
2027
years of professional experience

Work History

Flight Structural Load Engineer

Aeronautical Development Agency
02.2024 - Current
  • Developed a structural model for static aeroelasticity (SOL 144) in Nastran from the coefficient of pressure data from aerodynamic analysis.
  • Identified critical maneuver load cases by analyzing shear force, bending moment, and torsion moment across the fuselage and wing for stress monitoring.
  • Load cases are generated for various Mach numbers, across altitudes for various flight mass configurations.
  • Integrated stores to the aircraft for the required configuration load analysis.
  • Regulatory Awareness: A practical understanding of airworthiness standards for military aircraft, MIL-SPECs.
  • Proficient in MSC Nastran debugging and analysis in SOL 101, 103, 144.
  • Collaborated with cross-functional teams to streamline project workflows and ensure timely deliverables.

Aircraft Structural Optimization

02.2024 - Current
  • Performed composite wing skin panel optimization to achieve optimum weight while ensuring safety margins.
  • Constraint satisfaction: maintaining the material failure index under margin, protecting the panel from buckle, and ensuring the right aeroelastic efficiencies.
  • RESULTS from Modefrontier software: By pareto front analysis found three optimal design cases with balanced mass and displacement, saving 8% of total wing skin weight.

Stress Work

  • Global to Local FEA: Performed global to local structural analysis on aircraft wing and radome structures, transitioning load paths and force equilibrium from coarse GFEM to high-fidelity DFEM local models using HyperMesh, and executed modal and linear static analysis for integrity.
  • CAD-based mesh modification: updated existing meshes to reflect change orders and geometric updates directly from 3D models.

Education

B.E. - Aeronautical Engineering

Rajalakshmi Engineering College
Chennai
01.2023

HSC - Computer Science

SSKV Mat Hr Sec School
Kanchipuram
01.2019

Skills

  • Programming: MATLAB scripting, Python for automation, LaTeX for technical reports
  • Softwares: MSC NASTRAN (SOL 103, 105), MATLAB/Simulink, Python (NumPy, SciPy, Matplotlib), FEMAP, HyperMesh
  • Soft skills: Adaptability in fast paced work space,effective reporting ability

Timeline

Aircraft Structural Optimization

02.2024 - Current

Flight Structural Load Engineer

Aeronautical Development Agency
02.2024 - Current

HSC - Computer Science

SSKV Mat Hr Sec School

Stress Work

B.E. - Aeronautical Engineering

Rajalakshmi Engineering College
Haripriya K