Comparison of Test and Finite Element Analysis for Two Full-Scale Helicopter Crash Tests-Reference-Cited by-同舟云学术

Comparison of Test and Finite Element Analysis for Two Full-Scale Helicopter Crash Tests

Published:2011-04-04 Issue: Volume: Page:
ISSN:
Container-title:52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
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Author:

Annett Martin¹,Horta Lucas¹

Affiliation:

1. NASA Langley Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-1804

Reference33 articles.

1. 1Jackson,K.E.,Fuchs,Y.T.,andKellas,S."OverviewoftheNASASubsonicRotaryWingAeronauticsResearchProgram in Rotorcraft Crashworthiness," Journal of Aerospace Engineering, Special Issue on Ballistic Impact and Crashworthiness of AerospaceStructures,Volume22, No.3, July2009,pp.229-239.

2. 5Jackson, K. E., Fasanella, E. L., and Boitnott, R. L. "Full-Scale Crash Test and Finite Element Simulation of a Composite PrototypeHelicopter,"NASA/TP-2003-212641,2003.

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