標(biāo)題: Titlebook: Numerical Simulation of the Aerodynamics of High-Lift Configurations; Omar Darío López Mejia,Jaime A. Escobar Gomez Book 2018 Springer Int [打印本頁] 作者: detumescence 時間: 2025-3-21 16:07
書目名稱Numerical Simulation of the Aerodynamics of High-Lift Configurations影響因子(影響力)
書目名稱Numerical Simulation of the Aerodynamics of High-Lift Configurations影響因子(影響力)學(xué)科排名
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書目名稱Numerical Simulation of the Aerodynamics of High-Lift Configurations網(wǎng)絡(luò)公開度學(xué)科排名
書目名稱Numerical Simulation of the Aerodynamics of High-Lift Configurations被引頻次
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書目名稱Numerical Simulation of the Aerodynamics of High-Lift Configurations讀者反饋
書目名稱Numerical Simulation of the Aerodynamics of High-Lift Configurations讀者反饋學(xué)科排名
作者: Encumber 時間: 2025-3-22 00:12 作者: CHASE 時間: 2025-3-22 04:11
Omar Darío López Mejia,Jaime A. Escobar GomezDescribes state-of-the-art computational and theoretical models for simulation of high-lift configurations.Includes numerical results and validations of computational models applied to of high-lift co作者: Estrogen 時間: 2025-3-22 05:37
978-3-030-09671-7Springer International Publishing AG, part of Springer Nature 2018作者: synchronous 時間: 2025-3-22 12:09
Grid Generation About High-Lift Wing Configurations,about the NASA High Lift Common Research Model and the Japanese Aerospace Exploration Agency Standard Model with and without nacelles and pylons. Several modifications to the guidelines that enhance grid quality are presented. Additionally, the user-defined parameters within Pointwise that govern the mesh generation process are reviewed in detail.作者: 高興一回 時間: 2025-3-22 16:24
Book 2018voted to the Computational Fluids Dynamics (CFD) method using full Navier-Stokes solvers typically used in the simulation of high-lift configuration. With the increase of computational resources in the aeronautical industry, the computation of complex flows such as the aerodynamics of high-lift conf作者: GNAT 時間: 2025-3-22 19:58
Incompressible Solutions About High-Lift Wing Configurations,e incompressible solutions about the Japanese Aerospace Exploration Agency Standard Model configuration with and without nacelles and pylons are compared with experiment at multiple angles of attack to demonstrate the effectiveness of this approach.作者: 富饒 時間: 2025-3-22 23:04
lidations of computational models applied to of high-lift co.This book deals with numerical simulations and computations of the turbulent flow around high-lift configurations commonly used in aircraft. It is devoted to the Computational Fluids Dynamics (CFD) method using full Navier-Stokes solvers t作者: peritonitis 時間: 2025-3-23 02:07
numerical results and validation of these computational models. Finally, this book is a good reference for graduate students and researchers interested in the field of simulation of high-lift configurations..978-3-030-09671-7978-3-319-62136-4作者: Gerontology 時間: 2025-3-23 09:37 作者: 音樂戲劇 時間: 2025-3-23 10:25
A. Matiz-Chicacausa,C. A. Sedano up of an . In the third place it is recalled that independently of and long before TQM, statistics has been developing concepts and methods which have proved particularly fruitful in technical areas, like industrial research and production and process control, that are the core of any Quality System.作者: 整體 時間: 2025-3-23 15:13 作者: 土坯 時間: 2025-3-23 18:50 作者: 憎惡 時間: 2025-3-23 23:50
Time-Resolved Adaptive Direct FEM Simulation of High-Lift Aircraft Configurations, boundary-layer resolution. We introduce a numerical tripping-noise term to act as a seed for growth of perturbations; the results support that this triggers the correct physical separation at stall and has no significant pre-stall effect. We show that the methodology quantitavely and qualitatively 作者: Ingrained 時間: 2025-3-24 03:46 作者: 祖?zhèn)?nbsp; 時間: 2025-3-24 10:14
Book 2018putational models for simulation of high-lift configurations. It also shows and discusses numerical results and validation of these computational models. Finally, this book is a good reference for graduate students and researchers interested in the field of simulation of high-lift configurations..作者: 懶惰民族 時間: 2025-3-24 14:27 作者: 輕率的你 時間: 2025-3-24 18:03 作者: BRIDE 時間: 2025-3-24 22:50 作者: Grievance 時間: 2025-3-24 23:10 作者: ASSAY 時間: 2025-3-25 04:49 作者: PET-scan 時間: 2025-3-25 08:51
essentially on its organizational and formal aspects, with the intent of obtaining an official product/system registration in line with the ISO 9000 standards. The attention paid to statistical methods, which used to play a central role in any . some years ago, seems to have diminished. Thus in the 作者: 狼群 時間: 2025-3-25 14:15 作者: geriatrician 時間: 2025-3-25 16:48 作者: 諄諄教誨 時間: 2025-3-25 21:20
Johan Jansson,Ezhilmathi Krishnasamy,Massimiliano Leoni,Niclas Jansson,Johan Hoffmanut are satisfac- tory in terms of safety, length of working life and pride of ownership. In a manufacturing organization, therefore, the achievement of quality standards is not restricted to the production departments. It extends to all parts of the business from conceptual design to marketing, from作者: 種族被根除 時間: 2025-3-26 01:07 作者: Talkative 時間: 2025-3-26 06:44 作者: 高興一回 時間: 2025-3-26 10:50 作者: 濕潤 時間: 2025-3-26 15:27
Incompressible Solutions About High-Lift Wing Configurations,d industry alike. The compressible Navier–Stokes equations are usually used in these studies to predict the complex flow field generated by high lift wing configurations. However, since these configurations are applied in low-speed conditions where ., the compressible equations can exhibit some nume作者: 姑姑在炫耀 時間: 2025-3-26 17:15 作者: 完成 時間: 2025-3-27 00:58
Time-Resolved Adaptive Direct FEM Simulation of High-Lift Aircraft Configurations, a benchmark problem from the HiLiftPW-3 workshop to compute the flow past a JAXA Standard Model (JSM) aircraft model at realistic Reynolds numbers. The mesh is automatically constructed by the method as part of an adaptive algorithm based on a posteriori error estimation using adjoint techniques. N作者: Nucleate 時間: 2025-3-27 04:21 作者: AER 時間: 2025-3-27 05:28
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