Recent Development of Aerodynamic Design Methodologies, Kozo Fujii; George Dulikravich
Автор: Leifsson Leifur Et Al Название: Simulation-Driven Aerodynamic Design Using Variable-Fidelity Models ISBN: 1783266287 ISBN-13(EAN): 9781783266289 Издательство: World Scientific Publishing Рейтинг: Цена: 22810.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Computer simulations is a fundamental tool of the design process in many engineering disciplines including aerospace engineering.
Описание: This volume entitled "European Computational Aerodynamics Research Project (ECARP)" contains the contributions of partners presented in two work- shops focused on the following areas: Task 3 on Optimum Design and Task 4.2 on Navier Stokes Flow algorithms on Massively Parallel Processors. ECARP has been supported by the European Union (EU) through the Indus- trial and Materials Technology Programme, Area 3 Aeronautics, with the Third Research Framework Programme (1990-1994). Part A of this volume is focused on computational constrained optimization as a follow up of the EU research project" Optimum Design in Aerodynamics," (AERO-S9-0026) dealing with more viscous flow based real applications. It pro- vides the reader with a set of optimization tools and referenced data useful in modern aerodynamic design. Task 3 of the project entitled "Optimum Design" brought together 13 Euro- pean partners from the academic and industrial aeronautic oriented community showing state of the art expertise in traditional automated optimization software on current computer technology to improve the capability to optimize aircraft shapes.
Описание: Contains results of the German CFD initiative megadesign which combines CFD development activities from DLR, universities and aircraft industry. This title highlights improvements and enhancements of the flow solvers as well as developments with respect to aerodynamic and multidisciplinary shape optimization.
Описание: Reduction of Simulation Time.- Recent Developments of TAU Adaptation Capability.- Adaptive Wall Function for the Prediction of Turbulent Flows.- Acceleration of CFD Processes for Transport Aircraft.- Efficient Combat Aircraft Simulations with the TAU RANS Code.- Improvement of Simulation Quality.- Universal Wall Functions for Aerodynamic Flows: Turbulence Model Consistent Design, Potential and Limitations.- Computational Modelling of Transonic Aerodynamic Flows Using Near-Wall, Reynolds Stress Transport Models.- Transition Prediction for Three-Dimensional Configurations.- Application of Transition Prediction.- Numerical Simulation Quality Assessment for Transport Aircraft.- Fluid Structure Coupling.- Computational Methods for Aero-Structural Analysis and Optimisation of Aircrafts Based on Reduced-Order Structural Models.- Development and Application of TAU-ANSYS Coupling Procedure.- Fluid-Structure Coupling: Simplified Structural Model on Complex Configurations.- Improvement of Shape Optimization Strategies.- Development of an Automated Artificial Neural Network for Numerical Optimization.- modeFRONTIER(c), a Framework for the Optimization of Military Aircraft Configurations.- One-Shot Methods for Aerodynamic Shape Optimization.- Automatic Differentiation of FLOWer and MUGRIDO.- Adjoint Methods for Coupled CFD-CSM Optimization.- Aerodynamic and Multidisciplinary Optimization of 3D-Configurations.- Aerodynamic Optimization for Cruise and High-Lift Configurations.- Aerodynamic Optimization of an UCAV Configuration.- Flexible Wing Optimisation Based on Shapes and Structures.- Multidisciplinary Optimization of an UAV Combining CFD and CSM.
Описание: These Proceedings contain the papers and oral discussions presented at the Symposium on AERODYNAMIC DRAG MECHANISMS of Bluff Bodies and Road Vehides held at the General Motors Research Laboratories in Warren, Michigan, on September 27 and 28, 1976.
Автор: T. Cebeci Название: Numerical and Physical Aspects of Aerodynamic Flows ISBN: 3662126125 ISBN-13(EAN): 9783662126127 Издательство: Springer Рейтинг: Цена: 15672.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Автор: Lighthill M. J., Lighthill Sir M. J. Название: Higher Approximations in Aerodynamic Theory ISBN: 0691626014 ISBN-13(EAN): 9780691626017 Издательство: Wiley Рейтинг: Цена: 4752.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: Part of the Princeton Aeronautical Paperback series designed to bring to students and research engineers outstanding portions of the twelve-volume High Speed Aerodynamics and Jet Propulsion series. These books have been prepared by direct reproduction of the text from the original series and no attempt has been made to provide introductory material
Описание: Introduction.- Theory of Supercooled Liquids and Glasses.- Experimental Techniques.- Rare Earth Doped Barium Titanate Glass.- Liquid-Liquid Transitions in Y2O3-Al2O3.- Liquid Invar.- Indium Selenide.- Conclusions.
Автор: T. Cebeci Название: Numerical and Physical Aspects of Aerodynamic Flows II ISBN: 3662090163 ISBN-13(EAN): 9783662090169 Издательство: Springer Рейтинг: Цена: 15672.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: The Second Symposium on Numerical and Physical Aspects of Aerodynamic Flows was held at the California State University, Long Beach, January 17-20, 1983
Автор: Tuncer Cebeci Название: Numerical and Physical Aspects of Aerodynamic Flows IV ISBN: 3662026457 ISBN-13(EAN): 9783662026458 Издательство: Springer Рейтинг: Цена: 18284.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This volume contains a selection of the papers presented at the Fourth Symposium on Numerical and Physical Aspects of Aerodynamic Flows, which was held at the California State University, Long Beach, from 16-19 January 1989.
Автор: Claus Weiland Название: Aerodynamic Data of Space Vehicles ISBN: 3642541674 ISBN-13(EAN): 9783642541674 Издательство: Springer Рейтинг: Цена: 22203.00 р. Наличие на складе: Есть у поставщика Поставка под заказ.
Описание: This book details the aerodynamics of more than 25 vehicles. It provides readers with insight into the aerodynamics of various flight configurations.
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