Technical Paper

Finite Element Model Development and Test-Analysis Correlation for Two F28 Fuselage Section Drop Tests

SM_STRUCT_2017-2755

10/24/2017

Event
Rotorcraft Structures and Survivability - Hampton, Virginia 2017
Authors
Martin Annett NASA Langley Research Center
Karen Jackson NASA Langley Research Center
Justin Littell NASA Langley Research Center
Ian Haskin NASA Glenn Research Center
Abstract
Content

Finite Element Model Development and Test-Analysis Correlation for Two F28 Fuselage Section Drop Tests.

Meta Tags
Topics
Finite element analysis
Fuselages
Affiliated or Co-Author
NASA Langley Research Center
NASA Glenn Research Center
Details
DOI
https://doi.org/10.4050/SM_STRUCT_2017-2755
Citation
Annett, M., Jackson, K., Littell, J., and Haskin, I., "Finite Element Model Development and Test-Analysis Correlation for Two F28 Fuselage Section Drop Tests," Rotorcraft Structures and Survivability - Hampton, Virginia 2017, Hampton, Virginia, October 24, 2017, https://doi.org/10.4050/SM_STRUCT_2017-2755.
Additional Details
Publisher
The Vertical Flight Society
Published
10/24/2017
Product Code
SM_STRUCT_2017-2755
Content Type
Technical Paper
Language
English