Transient computational investigation on the ejection seat's aerodynamic coefficients at subsonic Mach number
In this study, the commercially available CFD software ANSYS-Fluent is used to conduct a
three-dimensional unsteady-state analysis of the aerodynamic coefficients of an ejection …
three-dimensional unsteady-state analysis of the aerodynamic coefficients of an ejection …
Enhancing the airfoil performance for a fixed-wing Martian aircraft
E Karpovich, T Kombaev - Aerospace Systems, 2024 - Springer
In this paper, a series of low-Reynolds number airfoils were explored in application to the
Long-Endurance Mars Exploration Flying Vehicle (LEMFEV) project. The end goal of the …
Long-Endurance Mars Exploration Flying Vehicle (LEMFEV) project. The end goal of the …
Airfoil Design and Performance Optimization of Rotorcraft Robots through the Integration of LSTM-PSO and Multilayer Perceptron Technologies
Z Li, Y Wang, H Zhou, X Wang - 2024 39th Youth Academic …, 2024 - ieeexplore.ieee.org
This study designs and employs the Long Short-Term Memory-Particle Swarm Optimization
(LSTM-PSO) algorithm, supplemented by a multilayer perceptron model, focusing on the …
(LSTM-PSO) algorithm, supplemented by a multilayer perceptron model, focusing on the …