Results are presented from the U.S. Army-Aerostructures Directorate/NASA-Langley Research Center joint research program on helicopter crashworthiness. Through the on-going research program an in-depth understanding was developed on the cause/effect relationships between material and architectural variables and the energy-absorption capability of composite material and structure. Composite materials were found to be efficient energy absorbers. Graphite/epoxy subfloor structures were more efficient energy absorbers than comparable structures fabricated from Kevlar or aluminum. An accurate method predicting the energy-absorption capability of beams was developed
During the 1960's over 30 full-scale aircraft crash tests were conducted by the Flight Safety Founda...
A design for a novel light-weight conical shaped energy absorbing (EA) composite subfloor structure ...
Thesis (Ph.D.)--University of Washington, 2014As fiber reinforced composite material systems become ...
This thesis presents an investigation into the progressive crushing of composite materials with the ...
Two composite energy absorbers were developed and evaluated at NASA Langley Research Center through ...
Considerable research interest has been directed towards the use of composite for crashworthiness a...
Modern helicopters make extensive use of composite materials to reduce structural weight. These incl...
A simple method of predicting the energy-absorption capability of composite subfloor beam structure ...
Failure behavior results are presented from crash dynamics research using concepts of aircraft eleme...
This paper provides an overview of rotorcraft crashworthiness research being conducted at NASA Langl...
This paper provides an overview of rotorcraft crashworthiness research being conducted at NASA Langl...
The experimental and analytical efforts being undertaken to investigate the response of composite an...
A new externally deployable energy absorbing system was demonstrated during a full-scale crash test ...
Two composite energy absorbers were developed and evaluated at NASA Langley Research Center through ...
Experimental and analytical results are presented which show the effect of floor placement on the st...
During the 1960's over 30 full-scale aircraft crash tests were conducted by the Flight Safety Founda...
A design for a novel light-weight conical shaped energy absorbing (EA) composite subfloor structure ...
Thesis (Ph.D.)--University of Washington, 2014As fiber reinforced composite material systems become ...
This thesis presents an investigation into the progressive crushing of composite materials with the ...
Two composite energy absorbers were developed and evaluated at NASA Langley Research Center through ...
Considerable research interest has been directed towards the use of composite for crashworthiness a...
Modern helicopters make extensive use of composite materials to reduce structural weight. These incl...
A simple method of predicting the energy-absorption capability of composite subfloor beam structure ...
Failure behavior results are presented from crash dynamics research using concepts of aircraft eleme...
This paper provides an overview of rotorcraft crashworthiness research being conducted at NASA Langl...
This paper provides an overview of rotorcraft crashworthiness research being conducted at NASA Langl...
The experimental and analytical efforts being undertaken to investigate the response of composite an...
A new externally deployable energy absorbing system was demonstrated during a full-scale crash test ...
Two composite energy absorbers were developed and evaluated at NASA Langley Research Center through ...
Experimental and analytical results are presented which show the effect of floor placement on the st...
During the 1960's over 30 full-scale aircraft crash tests were conducted by the Flight Safety Founda...
A design for a novel light-weight conical shaped energy absorbing (EA) composite subfloor structure ...
Thesis (Ph.D.)--University of Washington, 2014As fiber reinforced composite material systems become ...