|
|
|
|
|
Cesare Patuelli, Enrico Cestino and Giacomo Frulla
Vibration analysis of wing-box structures is a crucial aspect of the aeronautic design to avoid aeroelastic effects during normal flight operations. The deformation of a wing structure can induce nonlinear couplings, causing a different dynamic behavior ...
ver más
|
|
|
|
|
|
|
|
|
|
|
Alessandro Polla, Giacomo Frulla, Enrico Cestino, Raj Das and Pier Marzocca
The presented methodology offers the author?s view on how to bridge the gap between the numerical evaluation and physical response of a typical composite panel under high-velocity impact. A rational approach to failure conditions and progressive damage p...
ver más
|
|
|
|
|
|
|
|
|
|
|
Giorgio Capovilla, Enrico Cestino and Leonardo Reyneri
Current CubeSats usually exhibit a low structural mass efficiency and a low internal volume for their payloads. The present work aims to propose an advanced structural architecture for CubeSats that addresses the issues of low structural mass efficiency ...
ver más
|
|
|
|
|
|
|
|
|
|
|
Enrico Cestino, Davide Pisu, Vito Sapienza, Lorenzo Chesta and Valentina Martilla
A new Range Equation for a hybrid-electric propeller-driven aircraft was formulated by an original derivation based on the comparison of Virtual Electrical Aircraft (VEA) and Virtual Thermal Aircraft (VTA) range equations. The new formulation makes it po...
ver más
|
|
|
|
|
|
|
|
|
|
|
Enrico Cestino, Giacomo Frulla, Paolo Piana and Renzo Duella
Thin-walled composite box beam structural configuration is representative of a specific high aspect ratio wing structure. The optimal design procedure and lay-up definition including appropriate coupling necessary for aerospace applications has been iden...
ver más
|
|
|
|
|
|
|
|
|
|
|
Giorgio Capovilla, Enrico Cestino, Leonardo M. Reyneri and Giulio Romeo
CubeSats usually adopt aluminum alloys for primary structures, and a number of studies exist on Carbon Fiber Reinforced Plastic (CFRP) primary structures. The internal volume of a spacecraft is usually occupied by battery arrays, reducing the volume avai...
ver más
|
|
|
|
|
|
|
|
|
|
|
Alessandro Bacchini and Enrico Cestino
In the last ten years, different concepts of electric vertical take-off and landing aircrafts (eVTOLs) have been tested. This article addresses the problem of the choice of the best configuration. VTOLs built since the fifties are presented and their adv...
ver más
|
|
|
|
|
|