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Aerospace Engineering Final Year Topic: Investigation of Aircraft Landing Gear Energy Model

This Aerospace Engineering final year project investigates comparing fictional shock-absorption assumptions for an idealised landing using a non-operational civil aerospace model, permitted teaching data or explicitly fictional system evidence.

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Why choose this project topic?

The topic turns comparing fictional shock-absorption assumptions for an idealised landing into a bounded aerospace analysis with traceable assumptions. Comparing peak force, stroke and rebound gives a student a clear route to technical figures, model verification and a critical discussion of the gap between a teaching study and operational performance.

How do the selected aerospace modelling or system assumptions affect peak force, stroke and rebound when comparing fictional shock-absorption assumptions for an idealised landing?

Choose a documented teaching model or fictional civil aerospace case, then agree the parameter ranges and validation method for comparing fictional shock-absorption assumptions for an idealised landing.

Proposed project objectives

  1. 01Define the civil teaching model, assumptions and evidence needed for comparing fictional shock-absorption assumptions for an idealised landing.
  2. 02Use a documented mass-spring-damper model, vary damping and stiffness and inspect bounded vertical input scenarios.
  3. 03Compare peak force, stroke and rebound and document uncertainty and operational limits.

A suggested research approach

Use a documented mass-spring-damper model, vary damping and stiffness and inspect bounded vertical input scenarios. Confirm data permission and keep the work separate from operational flight systems. Record units and model validity ranges, verify calculations against a reference, and report peak force, stroke and rebound with sensitivity checks rather than presenting a single output as certified performance.

What you will need

  • Published teaching model
  • Fictional gear parameters
  • Dynamics solver

Keep your project scope clear

No drop test or real landing guidance is proposed and the model is not certification evidence.

Aerospace Engineering project chapter outline

Use this outline as a starting point. You can edit the chapter titles to match your department’s format during setup.

  1. Chapter 1Introduction
  2. Chapter 2Literature Review
  3. Chapter 3Theory and Methodology
  4. Chapter 4Results and Applications
  5. Chapter 5Summary, Conclusion and Recommendations

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