Progress and prospects of artificial intelligence development and applications in supersonic flow and combustion

J Le, M Yang, M Guo, Y Tian, H Zhang - Progress in Aerospace Sciences, 2024 - Elsevier
Due to the significant improvement in computing power and the rapid advancement of data
processing technologies, artificial intelligence (AI) has introduced new tools and …

Recent advances and prospects in hypersonic inlet design and intelligent optimization

Y Ma, M Guo, Y Tian, J Le - Aerospace Science and Technology, 2024 - Elsevier
As the “respiratory tract” of the air breathing engine, the hypersonic inlet plays the role of
compressing, decelerating, and pressurizing flow. However, research on the traditional inlet …

[HTML][HTML] URANOS: A GPU accelerated Navier-Stokes solver for compressible wall-bounded flows

F De Vanna, F Avanzi, M Cogo, S Sandrin… - Computer Physics …, 2023 - Elsevier
URANOS, a massively parallel GPU-accelerated compressible flow solver for high-fidelity
modeling of compressible wall flows, is presented. URANOS is based on modern high …

CFD modeling of wind turbine blades with eroded leading edge

M Carraro, F De Vanna, F Zweiri, E Benini, A Heidari… - Fluids, 2022 - mdpi.com
The present work compares 2D and 3D CFD modeling of wind turbine blades to define
reduced-order models of eroded leading edge arrangements. In particular, following an …

Numerical and experimental investigation on nosebleed air jet control for hypersonic vehicle

L Zhang, J Yang, T Duan, J Wang, X Li, K Zhang - Aerospace, 2023 - mdpi.com
A new idea of nosebleed air jets with strong coupled internal and external flow is put forward
using the lateral jet control principle to improve the maneuverability and fast reaction …

Aerodynamic design optimization of the hypersonic inward turning inlet in wide-speed range

F Qu, X Wang, J Zhong, H Qu - Physics of Fluids, 2024 - pubs.aip.org
A multipoint optimization based on the discrete adjoint optimization method in a wide-speed
range is carried out to improve the performance of the hypersonic inlet with a rectangular to …

Effect and mechanism of roughness on the performance of a five-stage axial flow compressor

Y Chen, C Gao, W Chu - Aerospace, 2022 - mdpi.com
In order to prolong the service life of multistage axial compressors, it is increasingly
important to study the influence of blade surface roughness on the compressor performance …

Numerical Assessment of a Two-Phase Model for Propulsive Pump Performance Prediction

F Avanzi, A Baù, F De Vanna, E Benini - Energies, 2023 - mdpi.com
The present work provides a detailed numerical investigation of a turbopump for waterjet
applications in cavitating conditions. In particular, the study focuses on the complexities of …

Research on 3d design of high-load counter-rotating Compressor based on aerodynamic optimization and CFD coupling method

T Yan, H Chen, J Fang, P Yan - Energies, 2022 - mdpi.com
In view of the flow instability problem caused by the strong shock wave and secondary flow
in the channel of the high-load counter-rotating compressor, this paper adopts the design …

Parametric research and aerodynamic characteristic of a two-stage transonic compressor for a turbine based combined cycle engine

H Shi - Aerospace, 2022 - mdpi.com
This paper researches the parametric optimization of a two-stage transonic compressor
having a large air bypass at partial rotating speed according to flow analysis for a turbine …