Jinting Xuan

Ms. Jinting Xuan

orcid

Research Focus & Metrics

Academic Career Length

2Years (2025-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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25 April 2025 in Drones
Verified
Journal Article
Open access
PDF file
MDMenglong Ding
Menglong Ding
HLHuadong Li
Huadong Li
LSLintao Shao
Lintao Shao
JXJinting Xuan
Jinting Xuan
CFChuanyan Feng
Chuanyan Feng
DBDawei Bie
Dawei Bie
Electric vertical take-off and landing (eVTOL) aircraft are transforming urban air mobility (UAM) by providing efficient, low-emission, and rapid transit in congested cities. However, ensuring safe and stable landings remains a critical challenge, particularly in constrained urban environments with variable wind conditions. This study investigates the landing aerodynamics of a multi-rotor eVTOL using the lattice Boltzmann method (LBM), a computational approach well-suited to complex boundary conditions and parallel processing. This analysis examines the ground effect, descent speed, and crosswind influence on lift distribution and stability. A rooftop landing scenario is also explored, where half of the rotors operate over a rooftop while the rest remain suspended in open air. Results indicate that rooftop landings introduce asymmetric lift distribution due to crosswind and roof-induced flow circulation, significantly increasing rolling moment compared to ground landings. These findings underscore the role of descent speed, crosswinds, and landing surface geometry in eVTOL aerodynamics, particularly the heightened risk of rollover in rooftop scenarios.

27 November 2025
Verified
Book Chapter
Open access
MDMenglong Ding
Menglong Ding
ZXZhaoyang Xu
Zhaoyang Xu
JXJinting Xuan
Jinting Xuan
YZYanyan Zhang
Yanyan Zhang
DBDawei Bie
Dawei Bie
LSLintao Shao
Lintao Shao
The aircraft wing beam serves as the primary load-bearing structure of an aircraft, and the quality of its cross-section design significantly impacts the aircraft’s performance, safety, and economic efficiency. Traditional design methods for wing beams often rely on experience and trial-and-error processes, which are not only time-consuming and labor-intensive but also result in low design efficiency and difficulty in achieving optimal results. Furthermore, conventional optimization algorithms lack transferability, requiring re-optimization for each design iteration. In contrast, reinforcement learning enhances the design process through trial-and-error learning and feedback mechanisms, improving both efficiency and quality. This study proposes a reinforcement learning-based multi-objective optimization design method for aircraft wing beam structures. The method facilitates multi-objective optimization, enables the storage of design knowledge, and allows for the future expansion of the design space.