Preliminary evaluation of thrust loss in commercial aircraft engine due to airborne collision with Unmanned Aerial Vehicles (UAVs)

This paper is devoted to investigating the influence of UAVs airborne collision with civil aircraft engine on the operation safety of commercial aircraft. The damage levels of the civil aircraft fan blades and compressor blades during the UAVs airborne collision are both evaluated based on the Finit...

Full description

Saved in:
Bibliographic Details
Main Authors: Mohd Hasrizam Che Man, Liu, Hu, Ng, Bing Feng, Low, Kin Huat
Other Authors: 2020 International Conference on Unmanned Aircraft Systems (ICUAS)
Format: Conference or Workshop Item
Language:English
Published: 2021
Subjects:
Online Access:https://hdl.handle.net/10356/148349
Tags: Add Tag
No Tags, Be the first to tag this record!
Institution: Nanyang Technological University
Language: English

Similar Items