This Website is not fully compatible with Internet Explorer.
For a more complete and secure browsing experience please consider using Microsoft Edge, Firefox, or Chrome

Use of Transient Dynamic Simulations for Damage Prediction of Aircraft Composite Structures for Bird Strike and Tyre debris Impacts

This extended abstract was submitted for the "NAFEMS India Conference 2025" Conference, held in Bengalura, India on 9-10 September, 2025.

Document Details

Referenceindia25-ext-abs-03
AuthorChaudhuri. A
LanguageEnglish
AudienceAnalyst
TypeExtended Abstract
Date 9th September 2025
OrganisationAirbus
RegionIndia

Download


Back to Previous Page