Add to ORKGThe impact analysis of composite aircraft structures is discussed. Topics discussed include: background remarks on aircraft crashworthiness; comments on modeling strategies for crashworthiness simulation; initial study of simulation of progressive failure of an aircraft component constructed of composite material; and research direction in composite characterization for impact analysis
NASA Langley Research Center obtained a composite helicopter cabin structure in 2010 from the US Arm...
Abstract: During the last years, criteria of automobile and aircraft projects have been more and mor...
The chapter presents the current state of the art in design, analysis and test of crashworthy compos...
The experimental and analytical efforts being undertaken to investigate the response of composite an...
The Landing and Impact Dynamics Branch of NASA Langley Research Center has been involved in impact d...
In the present paper, advanced numerical methodologies have been adopted to investigate the influenc...
This paper studies the ability of the fuselage's lower lobe to absorb the energy during a crash land...
The entry into service of the Boeing 787 and the Airbus A350 XWB heralded a new era in the utilisati...
An overview of failure behavior results is presented from some of the crash dynamics research conduc...
Failure behavior results are presented from crash dynamics research using concepts of aircraft eleme...
Damage tolerance is the most critical technical issue for composite fuselage structures studied in t...
The paper describes recent progress on the materials modelling and numerical simulation of the dynam...
A large number of full scale tests of general aviation aircraft, helicopters, and one unique air-to-...
The development of the latest generation of wide-body carbon-fibre composite passenger aircraft has ...
[[abstract]]This study analyzes the crashworthiness of a light aircraft that is constructed from com...
NASA Langley Research Center obtained a composite helicopter cabin structure in 2010 from the US Arm...
Abstract: During the last years, criteria of automobile and aircraft projects have been more and mor...
The chapter presents the current state of the art in design, analysis and test of crashworthy compos...
The experimental and analytical efforts being undertaken to investigate the response of composite an...
The Landing and Impact Dynamics Branch of NASA Langley Research Center has been involved in impact d...
In the present paper, advanced numerical methodologies have been adopted to investigate the influenc...
This paper studies the ability of the fuselage's lower lobe to absorb the energy during a crash land...
The entry into service of the Boeing 787 and the Airbus A350 XWB heralded a new era in the utilisati...
An overview of failure behavior results is presented from some of the crash dynamics research conduc...
Failure behavior results are presented from crash dynamics research using concepts of aircraft eleme...
Damage tolerance is the most critical technical issue for composite fuselage structures studied in t...
The paper describes recent progress on the materials modelling and numerical simulation of the dynam...
A large number of full scale tests of general aviation aircraft, helicopters, and one unique air-to-...
The development of the latest generation of wide-body carbon-fibre composite passenger aircraft has ...
[[abstract]]This study analyzes the crashworthiness of a light aircraft that is constructed from com...
NASA Langley Research Center obtained a composite helicopter cabin structure in 2010 from the US Arm...
Abstract: During the last years, criteria of automobile and aircraft projects have been more and mor...
The chapter presents the current state of the art in design, analysis and test of crashworthy compos...