Modern aerospace vehicles cannot be designed by optimizing each subsystem independently. Aerodynamics affects propulsion, propulsion affects structures, structures affect weight, and weight directly influences vehicle performance.
Multidisciplinary Design Optimization (MDO) provides a systematic engineering framework to integrate these disciplines and identify an optimized aerospace vehicle design.
This webinar introduces students, engineers, researchers, and aerospace enthusiasts to the fundamentals and practical applications of MDO in aircraft, UAVs, launch vehicles, rockets, and other aerospace systems
September 26, 2026
Saturday
7:00 pm-8 pm
No
MARS Exploration
hrmarsexplorationpvt@gmail.com
8530636474
Remote , Google Meet
After attending the webinar, participants will be able to:
✔ Explain the fundamentals of MDO
✔ Identify aerospace disciplines involved in multidisciplinary optimization
✔ Formulate basic aerospace optimization problems
✔ Understand objectives, variables, and constraints
✔ Explain the interaction between CFD, FEA, propulsion, and vehicle performance
✔ Understand optimization and design-space exploration
✔ Identify potential MDO applications in aerospace vehicle development
The aerospace industry increasingly relies on simulation-driven and optimization-driven design to develop lighter, safer, more efficient, and higher-performing vehicles.
Learning MDO helps engineers move from:
“Design → Analyze → Modify”
to:
“Model → Integrate → Optimize → Evaluate → Select.”
This systems-level approach is highly relevant to the future of aircraft, UAV, rockets, launch vehicles, and space transportation systems.
This webinar is suitable for:
No advanced MDO experience is required.
Shraddha Chandrasekaran is an aerospace engineering professional and researcher specializing in Multidisciplinary Design Optimization (MDO), aerodynamics, structures, propulsion, flight mechanics, CFD, and FEA.
She completed her B.E. in Aeronautical Engineering from Madras Institute of Technology (MIT), Anna University, followed by an M.Tech. in Aerospace Engineering from the Indian Institute of Science (IISc).
She has professional industry experience as an Engineer at Rolls-Royce, where she gained exposure to advanced aerospace engineering and engineering analysis.
Currently, she is working as a Senior Research Fellow at , ISRO, while pursuing her PhD in Aerospace Engineering at the Indian Institute of Space Science and Technology (IIST).
Her current research focuses on Multidisciplinary Design Optimization studies for drones/UAVs, integrating multiple aerospace disciplines to develop efficient and optimized vehicle designs.
Eligibility: 1 year to 4th year or completed BE/B Tech/ME/M Tech aerospace/aeronautical/ Mechanical Engineering or Bsc in AME / Aviation aeronautical/
Eligibility: 1 year to 4th year or completed BE/B Tech/ME/M Tech aerospace/aeronautical/ Mechanical Engineering or Bsc in AME / Aviation aeronautical/
Eligibility: 1 year to 4th year or completed BE/B Tech/ME/M Tech aerospace/aeronautical/ Mechanical Engineering or Bsc in AME / Aviation aeronautical/
Eligibility: 1 year to 4th year or completed BE/B Tech/ME/M Tech aerospace/aeronautical/ Mechanical Engineering or Bsc in AME / Aviation aeronautical/
Understand how Aerodynamics + Propulsion + Structures + Performance + Optimization come together to create better aerospace vehicles.
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