Application of the finite element method to predict the crashworthy response of a metallic helicopter under floor structure onto water-Reference-Cited by-同舟云学术

Application of the finite element method to predict the crashworthy response of a metallic helicopter under floor structure onto water

Published:2008-05 Issue:5 Volume:35 Page:347-362
ISSN:0734-743X
Container-title:International Journal of Impact Engineering
language:en
Short-container-title:International Journal of Impact Engineering

Author:

Hughes K.,Campbell J.,Vignjevic R.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Safety, Risk, Reliability and Quality,Aerospace Engineering,Automotive Engineering,Civil and Structural Engineering

Reference18 articles.

1. Von Karman Th. The impact of seaplane floats during landing. NACA Technical Note 321, October 1929.

2. Coltman JW, Neri LM. Analysis of US civil rotorcraft accidents for development of improved design criteria. National specialists meeting on crashworthy design of rotorcraft, American Helicopter Society, 1986.

3. Coltman JW, Domzalski L, Arndt SM. Evaluation of the crash environment for US Navy helicopters……the hazards and Navy response. National specialists meeting on crashworthy design of rotorcraft, American Helicopter Society, Atlanta, GA, 1986.

4. Chen CCT, Muller M, Fogary KM. Rotorcraft ditchings and water related impacts that occurred from 1982 to 1989—phase I. US Department of Transportation, FAA Technical Center, Atlantic City, DOT/FAA/CT-92/13, October 1993.

5. Muller M. Rotorcraft ditchings and water related impacts that occurred from 1982 to 1989—phase II. US Department of Transportation, FAA Technical Center, Atlantic City, DOT/FAA/CT-92/14, October 1993.

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