This paper presents a retrofit design of a subfloor structure for commuter aircrafts. The subfloor concept is developed to improve the crash safety and consists in adding to a conventional aluminum structure crushable elements made of foam-blocks. The finite element simulation of a 9 m/s vertical impact onto a rigid surface shows that the accelerations in correspondence of the seats and the occupants are limited to 22 g, in comparison to the 33 g of the original configuration. So, the maximum acceleration results 33% lower than the maximum one measured on the conventional subfloor. Also the floor buckling and the seat detachment are significantly reduced
A study has been conducted into the design of civil aircraft seats which are forward-facing and use ...
The paper describes recent progress on the materials modelling and numerical simulation of the dynam...
[[abstract]]In recent years, light sport aircraft, which not only serve the purpose of personal recr...
This paper presents a retrofit design of a subfloor structure for commuter aircrafts. The subfloor c...
o improve a helicopter design concept, which meets structural and crashworthiness requirements, a re...
The impact energy absorbing is a very important characteristic of an aircraft to enhance the surviva...
The present work was performed in the frame of a national research program focused on the developmen...
Crashworthiness of an aircraft fuselage and its structural components was investigated experimentall...
A 1/5-scale model composite fuselage concept for light aircraft and rotorcraft has been developed to...
This paper describes the MSC/DYTRAN crash simulation of a 1/5-scale model composite fuselage concept...
Within the framework of Brite-Euram programme CRASURV "Commercial Aircraft -Design for Crash Su...
This paper studies the crashworthiness characteristics of a fuselage section and its improvement. A ...
This paper studies the crashworthiness characteristics of a fuselage section and its improvement. A ...
Civil Aerospace Medical Institute1990PDFTech ReportGowdy, VanCivil Aeromedical InstituteUnited State...
Two types of energy absorbing passenger seat concepts suitable for installation in light twin-engine...
A study has been conducted into the design of civil aircraft seats which are forward-facing and use ...
The paper describes recent progress on the materials modelling and numerical simulation of the dynam...
[[abstract]]In recent years, light sport aircraft, which not only serve the purpose of personal recr...
This paper presents a retrofit design of a subfloor structure for commuter aircrafts. The subfloor c...
o improve a helicopter design concept, which meets structural and crashworthiness requirements, a re...
The impact energy absorbing is a very important characteristic of an aircraft to enhance the surviva...
The present work was performed in the frame of a national research program focused on the developmen...
Crashworthiness of an aircraft fuselage and its structural components was investigated experimentall...
A 1/5-scale model composite fuselage concept for light aircraft and rotorcraft has been developed to...
This paper describes the MSC/DYTRAN crash simulation of a 1/5-scale model composite fuselage concept...
Within the framework of Brite-Euram programme CRASURV "Commercial Aircraft -Design for Crash Su...
This paper studies the crashworthiness characteristics of a fuselage section and its improvement. A ...
This paper studies the crashworthiness characteristics of a fuselage section and its improvement. A ...
Civil Aerospace Medical Institute1990PDFTech ReportGowdy, VanCivil Aeromedical InstituteUnited State...
Two types of energy absorbing passenger seat concepts suitable for installation in light twin-engine...
A study has been conducted into the design of civil aircraft seats which are forward-facing and use ...
The paper describes recent progress on the materials modelling and numerical simulation of the dynam...
[[abstract]]In recent years, light sport aircraft, which not only serve the purpose of personal recr...