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...

Descripción completa

Guardado en:
Detalles Bibliográficos
Autores principales: Carmen Simona Paciello, Claudio Pezzella, Marika Belardo, Simone Magistro, Francesco Di Caprio, Vincenzo Musella, Giuseppe Lamanna, Luigi Di Palma
Formato: article
Lenguaje:EN
Publicado: MDPI AG 2021
Materias:
SPH
T
Q
Acceso en línea:https://doaj.org/article/8de0ca671a16452eaeb813763f20c105
Etiquetas: Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!