Research Catalog

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

Title
Development and calibration of a system-integrated rotorcraft finite element model for impact scenarios / Martin S. Annett [and four others].
Author
Annett, Martin S.
Publication
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2012.

Available Online

https://purl.fdlp.gov/GPO/gpo37521

Details

Additional Authors
Langley Research Center, issuing body.
Description
1 online resource (62 pages) : color illustrations.
Series Statement
NASA/TM ; 2012-217785
Uniform Title
NASA technical memorandum ; 2012-217785.
Subject
  • Helicopters
  • Crashworthiness
  • Impact loads
  • Finite element method
  • Calibrating
  • Rotary wing aircraft
Note
  • Title from title screen (viewed on June 17, 2013).
  • "November 2012."
Bibliography (note)
  • Includes bibliographical references (pages 60-62).
Funding (note)
  • Sponsored by National Aeronautics and Space Administration
Call Number
GPO Internet NAS 1.15:2012-217785
OCLC
marcive848927770
Author
Annett, Martin S., author.
Title
Development and calibration of a system-integrated rotorcraft finite element model for impact scenarios / Martin S. Annett [and four others].
Publisher
Hampton, Virginia : National Aeronautics and Space Administration, Langley Research Center, 2012.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA/TM ; 2012-217785
NASA technical memorandum ; 2012-217785.
Bibliography
Includes bibliographical references (pages 60-62).
Funding
Sponsored by National Aeronautics and Space Administration 877868.02.07.07.05.02.01
L-20199
Connect to:
https://purl.fdlp.gov/GPO/gpo37521
Added Author
Langley Research Center, issuing body.
Gpo Item No.
0830-D (online)
Sudoc No.
NAS 1.15:2012-217785
View in Legacy Catalog