Loads Development for two Aircraft Fuselages using FAR criteria and parametrised FE-models
Report
(2003)
Author(s)
PC Astori (TU Delft - System Engineering & Aircraft Design)
J. Hupperets (External organisation)
Michel Van Tooren (TU Delft - Old - LR Ch. System Integration: Aircraft Design)
Research Group
System Engineering & Aircraft Design
To reference this document use:
https://resolver.tudelft.nl/uuid:080718d5-6b4a-4356-b6bc-f49695d32dc1
More Info
expand_more
expand_more
Publication Year
2003
Research Group
System Engineering & Aircraft Design
Abstract
This report describes a preliminary structural analysis of 2 complete fuselages, both belonging to the jet airliner category and differing for passenger capacity: 100 and 350 passengers respectively; the analysis is done for a set of loading conditions considered relevant for the aircraft category, and is aimed to provide data for material selection for different areas of the fuselage.
No files available
Metadata only record. There are no files for this record.