Results 1 to 10 of about 12,489,898 (339)

Aerodynamic Design via Control Theory [PDF]

open access: yesJournal of Scientific Computing, 1988
The purpose of this paper is to propose that there are benefits in regarding the design problem as a control problem in which the control is the shape of the boundary. A variety of alternative formulations of the design problem can then be treated systematically by using the mathematical theory for control of systems governed by partial differential ...
A. Jameson
openaire   +3 more sources

Inverse Aerodynamic Design of Gas Turbine Blades using Probabilistic Machine Learning [PDF]

open access: yesJournal of Mechanical Design, 2021
One of the critical components in Industrial Gas Turbines (IGT) is the turbine blade. Design of turbine blades needs to consider multiple aspects like aerodynamic efficiency, durability, safety and manufacturing, which make the design process ...
Sayan Ghosh   +8 more
semanticscholar   +1 more source

Noise prediction research of a scaled turboprop aircraft

open access: yesXibei Gongye Daxue Xuebao, 2021
Aerodynamic noise level has become an important performance index of civil aircraft, and it is drawing more and more attention. Most airframe noise research based on CFD method is aimed at aircraft individual parts at present, while lack of noise ...
Song Minhua   +5 more
doaj   +1 more source

Aerodynamic Design, Analysis and Validation of a Small Blended-Wing-Body Unmanned Aerial Vehicle

open access: yesAerospace, 2022
This paper describes the aerodynamic design and assessment of a blended-wing–body (BWB) configuration under the distributed electric propulsion (DEP) installation constraints.
Kelei Wang, Zhou Zhou
semanticscholar   +1 more source

Research on flight load surrogate model using neural networks

open access: yesHangkong gongcheng jinzhan, 2023
In aircraft structural strength design, flight load analysis is required, but the load analysis cycle is long,so it is necessary to study more efficient and accurate flight load analysis methods to shorten the load design cycle.The horizontal tail of a ...
PENG Yuzhuo, TANG Zhen, XIAO Qizhi
doaj   +1 more source

Study on Aerodynamic Interference of Tanker Aircraft on Receiver Aircraft based on N-S Equations

open access: yesHangkong gongcheng jinzhan, 2022
The wake flow field of tanker aircraft can produce the complex flow interference on receiver aircraft during aerial refueling.The computational fluid dynamics(CFD)method based on Navier-Stokes(N-S)equations is used to analyze the wake flow field of the ...
GENG Yansheng   +3 more
doaj   +1 more source

Tools and methodologies for box-wing aircraft conceptual aerodynamic design and aeromechanic analysis

open access: yesMechanics & Industry, 2021
A way to face the challenge of moving towards a new greener aviation is to exploit disruptive aircraft architectures; one of the most promising concept is the PrandtlPlane, a box-wing aircraft based on the Prandtl's studies on multiplane lifting systems.
K. Abu Salem   +5 more
semanticscholar   +1 more source

High-dimensional aerodynamic data modeling using a machine learning method based on a convolutional neural network

open access: yesAdvances in Aerodynamics, 2022
Modeling high-dimensional aerodynamic data presents a significant challenge in aero-loads prediction, aerodynamic shape optimization, flight control, and simulation.
Bo-Wen Zan   +4 more
doaj   +1 more source

Efficient Global Aerodynamic Shape Optimization of a Full Aircraft Configuration Considering Trimming

open access: yesAerospace, 2023
Most existing aerodynamic shape optimization (ASO) studies do not take the balanced pitching moment into account and thus the optimized configuration has to be trimmed to ensure zero pitching moment, which causes additional drag and reduces the benefit ...
Kai Wang   +3 more
doaj   +1 more source

Multi-object aerodynamic design optimization using deep reinforcement learning

open access: yesAIP Advances, 2021
Aerodynamic design optimization is a key aspect in aircraft design. The further evolution of advanced aircraft derivatives requires a powerful optimization toolbox.
Xinyu Hui   +5 more
semanticscholar   +1 more source

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