Mathematical modeling and stability analysis of tiltrotor aircraft

H Sheng, C Zhang, Y Xiang - Drones, 2022 - mdpi.com
The key problem in the development process of a tiltrotor is its mathematical modeling.
Regarding that, this paper proposes a dividing modeling method which divides a tiltrotor into …

Aeroelastic tailoring of the next generation civil tiltrotor technological demonstrator composite wing

AD Marano, M Belardo, J Beretta, F Starace, S Orlando… - Aerospace, 2022 - mdpi.com
The tiltrotor wing structure is one of the most critical and heavily investigated structures in
design due to the fundamental need to consider the interactions between the wing, pylon …

High aspect ratio composite wings: geometrically nonlinear aeroelasticity, multi-disciplinary design optimization, manufacturing, and experimental testing

T Farsadi, M Ahmadi, M Sahin, H Haddad Khodaparast… - Aerospace, 2024 - mdpi.com
In the field of aerospace engineering, the design and manufacturing of high aspect ratio
composite wings has become a focal point of innovation and efficiency. These long, slender …

Non-Linear Analysis in Post-Buckling Regime of a Tilt Rotor Composite Wing Structure Using Detailed Model and Robust Loading Approach

A Chiariello, P Vitale, M Belardo, F Di Caprio… - Journal of Composites …, 2023 - mdpi.com
The design and development of a wing for a completely brand-new aircraft represents, in
aeronautics, one of the highest challenges from an engineering point of view. The present …

Two-Stage Intelligent Layout Design of Curved Cabin Door

T Gao, Z Xu, Z Li, P Liu, K Tian - Aerospace, 2023 - mdpi.com
As one of the most complex and critical components of spacecraft, the structural design of
the curved cabin door faces two challenges. On the one hand, it is difficult to obtain …

On numerical models for cube drop test of bladder fuel tank for aeronautical applications

D Cristillo, F Di Caprio, C Pezzella, C Paciello… - Journal of Composites …, 2022 - mdpi.com
For some categories of aircraft, such as helicopters and tiltrotors, fuel storage systems must
satisfy challenging crash resistance requirements in order to reduce or eliminate the …

Structural Scalability Preliminary Studies for the Next Generation Civil Tiltrotor Composite Wing

AD Marano, G Diodati, N Paletta, L Di Palma… - Aerospace, 2023 - mdpi.com
This paper is focused on structural scalability studies of a new generation of civil tiltrotor
wingbox structures. Starting from a reference wingbox, developed under the H2020 Clean …

On generating stiffening layouts with density-based topology optimization considering buckling

JF Gamache, A Vadean, N Dodane… - CEAS Aeronautical Journal, 2021 - Springer
This work includes a complete optimization, design, sizing and validation application of
density-based topology optimization for a single stiffened panel from the upper skin of a …

High Fidelity Crash Analysis of Ngctr-TD Composite Wing

L Di Palma, G Albo, M Nardone… - Journal of Physics …, 2024 - iopscience.iop.org
Open Access proceedings Journal of Physics: Conference series Page 1 Journal of Physics:
Conference Series PAPER • OPEN ACCESS High Fidelity Crash Analysis of Ngctr-TD …

Design process and environmental impact of unconventional tail airliners

A Sanchez-Carmona, C Cuerno-Rejado - Aerospace, 2021 - mdpi.com
The future of aviation depends on reducing the environmental impact of the aircraft.
Unconventional configurations can be the change the industry needs to achieve that goal …