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Job08 Apr 2026
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Mechanical Engineer - NVH – Senior Engineer

Tunga Aerospace
Location

One-Hub, Thiruporur, Tamil Nadu

Job type

Full time

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Job Description

Job Code: CoE-AS-MCF-M-003

Experience: 5 - 7 Years

Location: One-Hub, Thiruporur

No of Openings: 1

Date of Post: 03-Apr-2026

Applicants: 1


Apply directly at: https://www.tungasystems.com/apply.php?job=COE-AS-MCF-M-003
Preferred Experience

5–7 years of experience in NVH / vibration engineering

Strong fundamentals in structural dynamics and signal processing

Knowledge of environmental standards (DO-160, MIL-STD)

Familiarity with flight data analysis, correlation, and anomaly detection

Exposure to UAV or aerospace platforms preferred

Certification Awareness: Experience with aerospace qualification standards (DO-160, MIL-STD-810)

Reliability Engineering: Knowledge of fatigue, durability, and life prediction under vibration loads

Automation: Ability to develop automated scripts for vibration data processing and reporting

Innovation: Exposure to advanced damping materials and smart NVH solutions

Required Skill Sets & Tools
  • FEA: ANSYS Mechanical, Altair OptiStruct
  • NVH Tools: Simcenter 3D, Simcenter Testlab
  • Data: MATLAB, Python
  • Testing: Shaker table systems, acoustic measurement setups
Qualifications
Bachelor’s / Master’s in Mechanical / Aerospace Engineering
Key Responsibility Areas
  • Analysis & Simulation
    • Perform harmonic and random vibration analysis
    • Conduct Shock Response Spectrum (SRS) and modal analysis (FEA + experimental correlation)
    • Identify and mitigate resonance risks in UAV structures
  • Isolation & Design
    • Design vibration isolation systems (elastomer mounts, wire-rope isolators)
    • Optimize damping, stiffness, and transmissibility for critical components
  • Testing & Validation
    • Execute shaker table tests (sine, random, shock)
    • Conduct acoustic signature testing for UAV platforms
    • Perform modal testing and correlate results with simulation models
  • Signal Processing & Data Analysis
    • Analyze vibration data using FFT (Fast Fourier Transform) and PSD (Power Spectral Density)
    • Process flight log vibration data to extract frequency content, damping, and peak loads
    • Identify anomalies and recommend corrective design measures
  • Cross-Functional Collaboration
    • Work with structures team on stiffness tuning
    • Collaborate with mechanical design team on mounting strategies
    • Partner with avionics team to ensure component survivability under vibration loads
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