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عنوان
Numerical simulation of the aerodynamics of high-lift configurations /

پدید آورنده
Omar Darío López Mejia, Jaime A. Escobar Gomez, editors.

موضوع
Aerodynamics.,Computational fluid dynamics.,Lift (Aerodynamics),Aerodynamics.,Aerospace & aviation technology.,Computational fluid dynamics.,Computer modelling & simulation.,Fluid mechanics.,Lift (Aerodynamics),Maths for scientists.,Mechanics of fluids.,TECHNOLOGY & ENGINEERING-- Engineering (General),TECHNOLOGY & ENGINEERING-- Reference.

رده
TA357
.
5
.
D37

کتابخانه
Center and Library of Islamic Studies in European Languages

محل استقرار
استان: Qom ـ شهر: Qom

Center and Library of Islamic Studies in European Languages

تماس با کتابخانه : 32910706-025

INTERNATIONAL STANDARD BOOK NUMBER

(Number (ISBN
3030096718
(Number (ISBN
331962136X
(Number (ISBN
3319621378
(Number (ISBN
9783030096717
(Number (ISBN
9783319621364
(Number (ISBN
9783319621371
Erroneous ISBN
3319621351
Erroneous ISBN
9783319621357

TITLE AND STATEMENT OF RESPONSIBILITY

Title Proper
Numerical simulation of the aerodynamics of high-lift configurations /
General Material Designation
[Book]
First Statement of Responsibility
Omar Darío López Mejia, Jaime A. Escobar Gomez, editors.

.PUBLICATION, DISTRIBUTION, ETC

Place of Publication, Distribution, etc.
Cham, Switzerland :
Name of Publisher, Distributor, etc.
Springer,
Date of Publication, Distribution, etc.
2018.

PHYSICAL DESCRIPTION

Specific Material Designation and Extent of Item
1 online resource

INTERNAL BIBLIOGRAPHIES/INDEXES NOTE

Text of Note
Includes bibliographical references.

CONTENTS NOTE

Text of Note
Intro; Preface; Contents; Review on High-Lift Systems for Aerodynamic Applications; 1 Introduction; 2 Trailing Edge Devices; 3 Leading Edge Devices; 4 Physics of High-Lift Systems and Numerical Simulations; References; Grid Generation About High-Lift Wing Configurations; 1 Introduction; 2 CAD Model; 3 Mesh Generation Guidelines; 4 Surface Mesh Generation; 4.1 Farfield and Symmetry Plane; 4.2 Grid Quality; 4.3 Deviation from HiLiftPW3 Meshing Guidelines; 5 Volume Grid Generation; 6 Final Remarks; References; Incompressible Solutions About High-Lift Wing Configurations; 1 Introduction
Text of Note
2 Numerical Approach3 Grid Generation; 4 Solution Process; 5 Results and Discussion; 5.1 Force and Moment Comparisons; 5.2 Pressure Comparisons; 6 Conclusions and Future Work; References; Numerical Investigations of the Jaxa High-Lift Configuration Standard Model with MFlow Solver; 1 Introduction; 2 Geometry and Computational Grids; 3 Numerical Methods; 4 Results; 4.1 The Performance of Massively Parallel Computing; 4.2 The Effects of Nacelle and Pylon Assembled; 5 Conclusions; References; Time-Resolved Adaptive Direct FEM Simulation of High-Lift Aircraft Configurations; 1 Introduction
Text of Note
2 Simulation Methodology2.1 The cG(1)cG(1) Method; 2.2 The Adaptive Algorithm; 2.3 A Posteriori Error Estimate for cG(1)cG(1); 2.4 The Do-Nothing Error Estimate and Indicator; 2.5 Turbulent Boundary Layers; 2.6 Numerical Tripping; 2.7 The FEniCS-HPC Finite Element Computational Framework; 3 Results; 3.1 Aerodynamic Forces; 3.2 Pressure Coefficients; 3.3 Flow and Adaptive Mesh Refinement Visualization; 4 Conclusions; References; RANS Simulations of the High Lift Common Research Model with Open-Source Code SU2; 1 Introduction; 2 NASA's Common Research Model; 3 Numerical Methods
Text of Note
3.1 Stanford University Unstructured (SU2)3.2 Turbulence Modelling; 3.3 Computational Resources; 3.4 Geometry Description and Grids; 3.5 Geometry; 4 Results and Discussion; 5 Conclusions; References
0
8
8
8

SUMMARY OR ABSTRACT

Text of Note
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 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 configurations has become an active field not only in academic but also in industrial environments. The scope of the book includes applications and topics of interest related to the simulation of high-lift configurations such as: lift and drag prediction, unsteady aerodynamics, low Reynolds effects, high performance computing, turbulence modelling, flow feature visualization, among others. This book gives a description of the state-of-the-art of computational 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.

ACQUISITION INFORMATION NOTE

Source for Acquisition/Subscription Address
Springer Nature
Stock Number
com.springer.onix.9783319621364

OTHER EDITION IN ANOTHER MEDIUM

Title
Numerical simulation of the aerodynamics of high-lift configurations.
International Standard Book Number
3319621351

TOPICAL NAME USED AS SUBJECT

Aerodynamics.
Computational fluid dynamics.
Lift (Aerodynamics)
Aerodynamics.
Aerospace & aviation technology.
Computational fluid dynamics.
Computer modelling & simulation.
Fluid mechanics.
Lift (Aerodynamics)
Maths for scientists.
Mechanics of fluids.
TECHNOLOGY & ENGINEERING-- Engineering (General)
TECHNOLOGY & ENGINEERING-- Reference.

(SUBJECT CATEGORY (Provisional

TEC-- 009000
TEC-- 035000
TRP
TRP
TTDS
TTDS

DEWEY DECIMAL CLASSIFICATION

Number
620
.
1064

LIBRARY OF CONGRESS CLASSIFICATION

Class number
TA357
.
5
.
D37

PERSONAL NAME - ALTERNATIVE RESPONSIBILITY

Gomez, Jaime A. Escobar
Mejia, Omar Darío López

ORIGINATING SOURCE

Date of Transaction
20200823102022.0
Cataloguing Rules (Descriptive Conventions))
pn

ELECTRONIC LOCATION AND ACCESS

Electronic name
 مطالعه متن کتاب 

[Book]

Y

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