Results 81 to 90 of about 9,266,844 (203)
The basic tool set to design multi-stage axial compressors consists of fast codes for throughflow and blade-to-blade analysis. Detailed blade row design is conducted with 3D CFD, mainly to control the end wall flow.
Markus Schnoes +2 more
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Aerodynamic design optimization using flow feature parameterization
Design optimization methods using high-fidelity computational fluid dynamics simulations are becoming increasingly popular in the area of aerodynamic design, sustaining the desire to make these methods more computationally efficient.
Barrett, Thomas Robin
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Airfoil Preference and Adjustable Camber Impact Analysis for Trans-Medium Fixed-Wing Vehicles
The key to the realization of air-water trans-medium flight lies in the profile design of trans-medium flight and the satisfaction of different requirements of aerodynamic efficiency for air cruise and airfoil for underwater glide. In this paper, a trans-
Jixin LU +5 more
doaj +1 more source
Optimal airfoil design remains a critical challenge in aerodynamic engineering, with traditional methods requiring extensive computational resources and iterative processes.
Özlem Batur Dinler
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Recent advances in contrastive language‒image pretraining (CLIP) models and generative AI have demonstrated significant capabilities in cross-modal understanding and content generation. Based on these developments, this study introduces a novel framework
Mingcheng Lei, Yufei Zhang
doaj +1 more source
Transonic Buffet Suppression by Airfoil Optimization
The main buffet suppression techniques of aircrafts include active and passive flow control, aiming to reduce the impact of the fluctuating loads on the airfoil. These techniques are remedies after the airfoil design. The buffet suppression is not always
Yiming Gong +2 more
doaj +1 more source
Under complex flight conditions, such as obstacle avoidance and extreme sea state, wing-in-ground (WIG) effect aircraft need to ascend to higher altitudes, resulting in the disappearance of the ground effect.
WANG Chenlu +6 more
doaj +1 more source
Calculation and uncertainty analysis method for airfoil drag coefficient considering compressibility
In order to meet the need of evaluating the effectiveness of airfoil drag reduction design, the calculation and uncertainty analysis method for airfoil drag coefficient considering compressibility is studied.
Yufeng Du +4 more
doaj +1 more source
Airfoil Design Using Genetic Algorithms
Genetic algorithms (GAs) are a search method used in finding true or approximate solutions to optimization and search problems. They have been applied in different fields like computer science, engineering, and economics. Here, we apply GA to the problem of designing a symmetric airfoil with high lift coefficient. Each population member, or chromosome,
openaire +3 more sources
Effects of turbulence modelling on the analysis and optimisation of high-lift configurations [PDF]
Due to the significant effects on the performance and competitiveness of aircraft, high lift devices are of extreme importance in aircraft design. The flow physics of high lift devices is so complex, that traditional one pass and multi-pass design ...
Guo, Chuanliang.
core

