Cover image for Aerodynamics for engineers
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:

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30000010177919 TL570 B42 2009 Open Access Book Book
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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.