Aerodynamics for Engineering Students (Record no. 32430)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 04501nam a22001937a 4500 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | OSt |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| International Standard Book Number | 9789382291176 |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 629.1323 |
| Item number | HOU-A |
| 100 ## - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Houghton, E L |
| 245 ## - TITLE STATEMENT | |
| Title | Aerodynamics for Engineering Students |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 6th |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) | |
| Place of publication, distribution, etc | New Delhi |
| Name of publisher, distributor, etc | Elesveier |
| Date of publication, distribution, etc | 2013 |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 723p. |
| 500 ## - GENERAL NOTE | |
| General note | Table of Contents<br/>PART I: INTRODUCTION<br/><br/>CHAPTER 1 Basic Concepts and Definitions <br/>1.1 Introduction <br/>1.2 Units and Dimensions <br/>1.3 Relevant Properties <br/>1.4 Aeronautical Definitions <br/>1.5 Dimensional Analysis <br/>1.6 Basic Aerodynamics <br/>1.7 Control-volume Analysis<br/>1.8 Aerodynamics Around Us <br/>1.9 Exercises<br/><br/>PART II: FUNDAMENTALS OF FLUID MECHANICS<br/><br/>CHAPTER 2 Equations of Motion<br/>2.1 Introduction <br/>2.2 One-Dimensional Flow: The Basic Equations <br/>2.3 Viscous Boundary Layers<br/>2.4 Measurement of Air Speed <br/>2.5 Two-Dimensional Flow <br/>2.6 Stream Function and Streamline <br/>2.7 Momentum Equation <br/>2.8 Rates of Strain, Rotational Flow, and Vorticity<br/>2.9 Navier-Stokes Equations <br/>2.10 Properties of the Navier-Stokes Equations <br/>2.11 Exact Solutions of the Navier-Stokes Equations <br/>2.12 Aerodynamics Around Us<br/>2.13 Exercises<br/><br/>CHAPTER 3 Viscous Boundary Layers <br/>3.1 Introduction <br/>3.2 Prandtl’s Boundary-Layer Equations <br/>3.3 Similarity Solutions<br/>3.4 Boundary-Layer Separation <br/>3.5 Flow Past Cylinders and Spheres <br/>3.6 The Momentum-Integral Equation <br/>3.7 Approximate Methods for a Boundary Layer on a Flat Plate with Zero Pressure Gradient <br/>3.8 Additional Examples of the Momentum-Integral Equation <br/>3.9 Laminar-Turbulent Transition <br/>3.10 The Physics of Turbulent Boundary Layers<br/>3.11 Exercises<br/><br/>CHAPTER 4 Compressible Flow <br/>4.1 Introduction <br/>4.2 Isentropic One-Dimensional Flow <br/>4.3 One-Dimensional Flow: Weak Waves <br/>4.4 One-Dimensional Flow: Plane Normal Shock Waves <br/>4.5 Mach Waves <br/>4.6 Shock Waves <br/>4.7 Some Boundary-Layer Effects in Supersonic Flow <br/>4.8 Exercises<br/><br/>PART III: AERODYNAMICS OF WINGS AND BODIES<br/><br/>CHAPTER 5 Potential Flow <br/>5.1 Two-Dimensional Flows <br/>5.2 Standard Flows in Terms of the vVelocity Potential and Stream Function <br/>5.3 Axisymmetric Flows (Inviscid and Incompressible Flows) <br/>5.4 Computational (Panel) Methods <br/>5.5 Exercises <br/><br/>CHAPTER 6 Two-Dimensional Wing Theory <br/>6.1 Introduction <br/>6.2 The Development of Airfoil Theory <br/>6.3 General Thin-Airfoil Theory <br/>6.4 Solution to the General Equation <br/>6.5 The Flapped Airfoil <br/>6.6 The Jet Flap <br/>6.7 Normal Force and Pitching Moment Derivatives Due to Pitching <br/>6.8 Particular Camber Lines <br/>6.9 The Thickness Problem for Thin-Airfoil Theory <br/>6.10 Computational (Panel) Methods for Two-Dimensional Lifting Flows <br/>6.11 Exercises <br/><br/>CHAPTER 7 Wing Theory <br/>7.1 The Vortex System <br/>7.2 Laws of Vortex Motion <br/>7.3 The Wing as a Simplified Horseshoe Vortex <br/>7.4 Vortex Sheets <br/>7.5 Relationship between Spanwise Loading and Trailing Vorticity <br/>7.6 Determination of Load Distribution on a Given Wing <br/>7.7 Swept and Delta Wings <br/>7.8 Computational (Panel) Methods for Wings <br/>7.9 Exercises <br/><br/>CHAPTER 8 Airfoils and Wings in Compressible Flow <br/>8.1 Wings in Compressible Flow <br/>8.2 Exercises <br/><br/>PART IV: APPLICATIONS OF AERODYNAMICS<br/><br/>CHAPTER 9: Computational Fluid Dynamics<br/>9.1 Computational Methods <br/>9.2 Estimation of Profile Drag from the Velocity Profile in a Wake <br/>9.3 Application of Commercially Available Tools (Issues Confronted by Users)<br/>9.4 Exercises<br/><br/>CHAPTER 10 Flow Control, Planar and Rotating Wing Designs <br/>10.1 Introduction <br/>10.2 Maximizing Lift for Single-Element Airfoils <br/>10.3 Multi-Element Airfoils <br/>10.4 Boundary Layer Control Prevention to Separation <br/>10.5 Reduction of Skin-Friction Drag <br/>10.6 Reduction of Form Drag <br/>10.7 Reduction of Induced Drag <br/>10.8 Low-speed Aircraft Design Considerations <br/>10.9 Propeller and Rotorcraft Blades <br/>10.10 Reduction of Wave Drag<br/>10.11 Exercises<br/><br/>Appendix A: Symbols and Notation <br/>Appendix B: Properties of Standard Atmosphere <br/>Appendix C: A Solution of Glauert Type Integrals <br/>Appendix D: Conversion of Imperial Units to Syst´eme International (SI) Units |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | Other branches of engineering |
| 856 ## - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="https://books.google.co.in/books?id=4YCThwzeTBQC&printsec=frontcover&dq=Aerodynamics+for+Engineering+Students&hl=en&sa=X&ved=0ahUKEwij39SC-ufhAhXWWisKHaKzDsEQ6AEILjAB#v=onepage&q=Aerodynamics%20for%20Engineering%20Students&f=false">https://books.google.co.in/books?id=4YCThwzeTBQC&printsec=frontcover&dq=Aerodynamics+for+Engineering+Students&hl=en&sa=X&ved=0ahUKEwij39SC-ufhAhXWWisKHaKzDsEQ6AEILjAB#v=onepage&q=Aerodynamics%20for%20Engineering%20Students&f=false</a> |
| 901 ## - LOCAL DATA ELEMENT A, LDA (RLIN) | |
| Acc. No. | 21099 |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Source of classification or shelving scheme | Dewey Decimal Classification |
| Koha item type | Books |
| Withdrawn status | Lost status | Source of classification or shelving scheme | Damaged status | Not for loan | Collection code | Home library | Current library | Shelving location | Date acquired | Cost, normal purchase price | Total Checkouts | Full call number | Barcode | Date last seen | Uniform Resource Identifier | Price effective from | Koha item type | Date last borrowed |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Dewey Decimal Classification | Not For Loan | Reference | Amity Central Library | Amity Central Library | ASET Aerospace | 09/10/2014 | 565.00 | 629.1323 HOU-A | 21099 | 09/10/2014 | https://epgp.inflibnet.ac.in/UploadedContent.php | 09/10/2014 | Reference Book | |||||
| Dewey Decimal Classification | Amity Central Library | Amity Central Library | ASET Aerospace | 09/10/2014 | 565.00 | 4 | 629.1323 HOU-A | 21100 | 22/07/2016 | https://epgp.inflibnet.ac.in/UploadedContent.php | 09/10/2014 | Books | 09/05/2016 | |||||
| Dewey Decimal Classification | Amity Central Library | Amity Central Library | ASET Aerospace | 09/10/2014 | 565.00 | 3 | 629.1323 HOU-A | 21101 | 11/10/2018 | https://epgp.inflibnet.ac.in/UploadedContent.php | 09/10/2014 | Books | 25/04/2018 |