Development and calibration of a system-integrated rotorcraft finite element model for impact scenarios /

Bibliographic Details

Main Author:	Annett, Martin S. (Author)
Format:	Government Document eBook
Language:	English
Published:	Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2012.
Series:	NASA technical memorandum ; 2012-217785.
Subjects:	Helicopters. Crashworthiness. Impact loads. Finite element method. Calibrating. Rotary wing aircraft.
Online Access:	https://purl.fdlp.gov/GPO/gpo37521