Crashworthiness of a Composite Bladder Fuel Tank for a Tilt Rotor Aircraft
The fulfilment of the crash is a demanding requirement for a Tiltrotor. Indeed, such a kind of aircraft, being a hybrid between an airplane and a helicopter, inherits the requirements mainly from helicopters (EASA CS 29) due to its hovering ability. In particular, the fuel storage system must be des...
Main Authors: | Carmen Simona Paciello, Claudio Pezzella, Marika Belardo, Simone Magistro, Francesco Di Caprio, Vincenzo Musella, Giuseppe Lamanna, Luigi Di Palma |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2021-10-01
|
Series: | Journal of Composites Science |
Subjects: | |
Online Access: | https://www.mdpi.com/2504-477X/5/11/285 |
Similar Items
-
On Numerical Models for Cube Drop Test of Bladder Fuel Tank for Aeronautical Applications
by: Domenico Cristillo, et al.
Published: (2022-03-01) -
Modelling and Simulation in High-Fidelity Crash Analysis of NGCTR-TD Composite Wing
by: Luigi Di Palma, et al.
Published: (2024-02-01) -
Autonomous tilt-rotor UAV
by: Chao, Joshua Jang En
Published: (2013) -
Finite element analysis for crashworthiness of automotive side door reinforcement
by: Farhaninejad, Ali
Published: (2014) -
Wind Disturbance Rejection Control Of Tilt Rotor Aircraft In Transition Phase Based On Improved Active Disturbance Rejection Control
by: Liben Yang, et al.
Published: (2023-04-01)