Title:
Aerodynamics for engineers
Personal Author:
Edition:
5th ed.
Publication Information:
New York, NY. : Prentice Hall, 2009
Physical Description:
xx, 732 p. : ill. ; 24 cm.
ISBN:
9780132272681
Subject Term:
Added Author:
Available:*
Library | Item Barcode | Call Number | Material Type | Item Category 1 | Status |
---|---|---|---|---|---|
Searching... | 30000010177919 | TL570 B42 2009 | Open Access Book | Book | Searching... |
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Summary
Summary
Revised to reflect the technological advances and modern application in aerodynamics, this edition merges fundamental fluid mechanics, experimental techniques, and computational fluid dynamics techniques to build a solid foundation for students in aerodynamic applications from low-speed flight through hypersonic flight.
Table of Contents
1 Fluid Properties |
Concept of a Fluid |
Fluid as a Continuum |
Fluid Properties |
Pressure Variation in a Static Fluid Medium |
The Standard Atmosphere |
2 Fundamentals of Fluid Mechanics |
Introduction to Fluid Dynamics |
Conservation of Mass |
Conservation of Linear Momentum |
Applications to Constant-Property Flows |
Reynolds Number and Mach Number as Similarity Parameters |
Concept of the Boundary Layer |
Conservation of Energy |
First Law of Thermodynamics |
Derivation of the Energy Equation |
3 Dynamics of an Incompressible, Inviscid Flow Field |
Inviscid Flows |
Bernoulli's Equation |
Use of Bernoulli's Equation to Determine Airspeed |
The Pressure Coefficient |
Circulation |
Irrotational Flow |
Kelvin's Theorem |
Incompressible, Irrotational Flow |
Stream Function in a Two-Dimensional, Incompressible Flow |
Relation Between Streamlines and Equipotential Lines |
Superposition of Flows |
Elementary Flows |
Adding Elementary Flows to Describe Flow Around a Cylinder |
Lift and Drag Coefficients as Dimensionless Flow-Field Parameters |
Flow Around a Cylinder with Circulation |
Source Density Distribution on the Body Surface |
Incompressible, Axisymmetric Flow |
4 Viscous Boundary Layers |
Equations Governing the Boundary Layer for a Steady, Two-Dimensional, Incompressible Flow |
Boundary Conditions |
Incompressible, Laminar Boundary Layer |
Boundary-Layer Transition |
Incompressible, Turbulent Boundary Layer |
Eddy Viscosity and Mixing Length Concepts |
Integral Equations for a Flat-Plate Boundary Layer |
Thermal Boundary Layer for Constant-Property Flows |
5 Characteristic Parameters for Airfoil and Wing Aerodynamics |
Characterization of Aerodynamic Forces and Moments |
Airfoil Geometry Parameters |
Wing-Geometry Parameters |
Aerodynamic Force and Moment Coefficients |
Wings of Finite Span |
6 Incompressible Flows around Airfoils of Infinite Span |
General Comments |
Circulation and the Generation of Lift |
General Thin-Airfoil Theory |
Thin, Flat-Plate Airfoil (Symmetric Airfoil). Thin, Cambered Airfoil |
High-Lift Airfoil Sections |
Multielement Airfoil Sections for Generating High Lift |
High-Lift Military Airfoils |
7 Incompressible Flows about Wings of Finite Span |
General Comments |
Vortex System |
Lifting-Line Theory for Unswept Wings |
Panel Methods |
Vortex Lattice Method |
Factors Affecting Drag Due-to-Lift at Subsonic Speeds |
Delta Wings |
Leading-Edge Extensions |
Asymmetric Loads on the Fuselage at High Angles of Attack |
Flow Fields for Aircraft at High Angles of Attack |
8 Dynamics of a Compressible Flow Field |
Thermodynamic Concepts |
Adiabatic Flow in a Variable-Area Streamtube |
Isentropic Flow in a Variable-Area |
Characteristic Equations and Prandtl-Meyer Flow |
Shock Waves |
Viscous Boundary Layer |
9 Compressible, Subsonic Flows and Transonic Flows |
Compressible, Subsonic Flow |
Transonic Flow Past Unswept Airfoils |
Swept Wings at Transonic Speeds |
Forward Swept Wing |
Transonic Aircraft |
10 Two-Dimensional Supersonic Flows around Thin Airfoil |
Linear Theory |
Second-Order Theory (Busemann's Theory). Shock-Expansion Technique |
11 Supersonic Flows Over Wings and Airplane Configurations |
General Remarks About Lift and Drag |
General Remarks About Supersonic Wings |
Governing Equation and Boundary Conditions |
Consequences of Linearity |
Solution Methods |
Conical-Flow Method |
Singularity-Distribution Method |
Design Considerations for Supersonic Aircraft |
Some Comments About the Design of the SST and of the HSCT. Aerodynamic Interaction |
Aerodynamic Analysis for Complete Configurations in a Supersonic Stream |
12 Hypersonic Flows. |