20   Artículos

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en línea
Jiangtao Chen, Jiao Zhao, Wei Xiao, Luogeng Lv, Wei Zhao and Xiaojun Wu    
Given the randomness inherent in fluid dynamics problems and limitations in human cognition, Computational Fluid Dynamics (CFD) modeling and simulation are afflicted with non-negligible uncertainties, casting doubts on the credibility of CFD. Scientifica... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mario Carta, Tiziano Ghisu and Shahrokh Shahpar    
Due to the increasingly high turbine inlet temperatures, heat transfer analysis is now, more than ever, a vital part of the design and optimization of high-pressure turbine rotor blades of a modern jet engine. The present study aimed to find out how shap... ver más

 
en línea
Emanuele Spinosa, Riccardo Pellegrini, Antonio Posa, Riccardo Broglia, Mario De Biase and Andrea Serani    
The paper presents the use of a supervised active learning approach for the solution of a simulation-driven design optimization (SDDO) problem, pertaining to the resistance reduction of a destroyer-type vessel in calm water. The optimization is formulate... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Markus P. Rumpfkeil, Dean Bryson and Phil Beran    
In this article, multi-fidelity kriging and sparse polynomial chaos expansion (SPCE) surrogate models are constructed. In addition, a novel combination of the two surrogate approaches into a multi-fidelity SPCE-Kriging model will be presented. Accurate s... ver más
Revista: Algorithms    Formato: Electrónico

 
en línea
Andrew S. Thelen, Dean E. Bryson, Bret K. Stanford and Philip S. Beran    
The simultaneous optimization of aircraft shape and internal structural size for transonic flight is excessively costly. The analysis of the governing physics is expensive, in particular for highly flexible aircraft, and the search for optima using analy... ver más
Revista: Algorithms    Formato: Electrónico

 
en línea
Sihmehmet Yildiz, Hayriye Pehlivan Solak and Melike Nikbay    
Uncertainty quantification has proven to be an indispensable study for enhancing reliability and robustness of engineering systems in the early design phase. Single and multi-fidelity surrogate modelling methods have been used to replace the expensive hi... ver más
Revista: Algorithms    Formato: Electrónico

 
en línea
Angelos Kafkas, Spyridon Kilimtzidis, Athanasios Kotzakolios, Vassilis Kostopoulos and George Lampeas    
Efficient optimization is a prerequisite to realize the full potential of an aeronautical structure. The success of an optimization framework is predominately influenced by the ability to capture all relevant physics. Furthermore, high computational effi... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Stanislav Karpuk, Yaolong Liu and Ali Elham    
The German Cluster of Excellence SE²A (Sustainable and Energy Efficient Aviation) is established in order to investigate the influence of game-changing technologies on the energy efficiency of future transport aircraft. In this paper, the preliminary inv... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Aldo Serafino, Benoit Obert and Paola Cinnella    
Efficient Robust Design Optimization (RDO) strategies coupling a parsimonious uncertainty quantification (UQ) method with a surrogate-based multi-objective genetic algorithm (SMOGA) are investigated for a test problem in computational fluid dynamics (CFD... ver más
Revista: Algorithms    Formato: Electrónico

 
en línea
Diwakar Singh, Antonios F. Antoniadis, Panagiotis Tsoutsanis, Hyo-Sang Shin, Antonios Tsourdos, Samuel Mathekga and Karl W. Jenkins    
This paper introduces a multi-fidelity computational framework for the analysis of aerodynamic performance of flight formation. The Vortex Lattice and Reynolds Averaged Navier–Stokes methods form the basis of the framework, as low- and high-fidelit... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Diwakar Singh, Antonios F. Antoniadis, Panagiotis Tsoutsanis, Hyo-Sang Shin, Antonios Tsourdos, Samuel Mathekga and Karl W. Jenkins    
This paper introduces a multi-fidelity computational framework for the analysis of aerodynamic performance of flight formation. The Vortex Lattice and Reynolds Averaged Navier?Stokes methods form the basis of the framework, as low- and high-fidelity, res... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Atthaphon Ariyarit and Masahiro Kanazaki    
In this study, efficient global optimization (EGO) with a multi-fidelity hybrid surrogate model for multi-objective optimization is proposed to solve multi-objective real-world design problems. In the proposed approach, a design exploration is carried ou... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Vinh Pham, Maxim Tyan, Tuan Anh Nguyen and Jae-Woo Lee    
Multi-fidelity surrogate modeling (MFSM) methods are gaining recognition for their effectiveness in addressing simulation-based design challenges. Prior approaches have typically relied on recursive techniques, combining a limited number of high-fidelity... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Saurabh Mittal, Robert L. Wittman, John Gibson, Josh Huffman and Hans Miller    
Autonomous and AI-enabled systems present a challenge for integration within the System of Sys-tems (SoS) paradigm. A full system of systems (SoS) testbed is necessary to verify the integrity of a given system and preserve the modularization and accounta... ver más
Revista: Information    Formato: Electrónico

 
en línea
Mengmeng Zhang, Aidan Jungo, Alessandro Augusto Gastaldi and Tomas Melin    
This paper discusses multi-fidelity aircraft geometry modeling and meshing with the common language schema CPACS. The CPACS interfaces are described, and examples of variable fidelity aerodynamic analysis results applied to the reference aircraft are pre... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mengmeng Zhang, Aidan Jungo, Alessandro Augusto Gastaldi and Tomas Melin    
This paper discusses multi-fidelity aircraft geometry modeling and meshing with the common language schema CPACS. The CPACS interfaces are described, and examples of variable fidelity aerodynamic analysis results applied to the reference aircraft are pre... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Mohsen Rostami, Julian Bardin, Daniel Neufeld and Joon Chung    
Recent development in Electric Vertical Take-off and Landing (eVTOL) aircraft makes it a popular design approach for urban air mobility (UAM). When designing these configurations, due to the uncertainty present in semi-empirical estimations, often used f... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Stanislav Karpuk, Yiyuan Ma and Ali Elham    
Present work investigates the potential of a long-range commercial blended wing body configuration powered by hydrogen combustion engines with future airframe and propulsion technologies. Future technologies include advanced materials, load alleviation t... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Stanislav Karpuk, Rolf Radespiel and Ali Elham    
The present work demonstrates the impact of future airframe and propulsion technologies on the sustainability of potential future medium-range commercial jets with design specifications similar to the Airbus A320-200. Advanced airframe and engine technol... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Karim Abu Salem, Vittorio Cipolla, Giuseppe Palaia, Vincenzo Binante and Davide Zanetti    
The introduction of disruptive innovations in the transport aviation sector is becoming increasingly necessary. This is because there are many very demanding challenges that the transport aviation system will have to face in the years ahead. In particula... ver más
Revista: Aerospace    Formato: Electrónico

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