(Ebook) Aerodynamics for Engineers 1st Edition by John J Bertin, Russell M Cummings ISBN 9780273793274 0273793276

(Ebook) Aerodynamics for Engineers 1st Edition by John J Bertin, Russell M Cummings ISBN 9780273793274 0273793276

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Product details:

ISBN 10: 0273793276
ISBN 13: 9780273793274
Author: John J Bertin, Russell M Cummings

(Ebook) Aerodynamics for Engineers 1st Edition Table of contents:

1. Introduction

• Solving for the Aerothermodynamic Parameters

• Description of an Airplane

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 and the Velocity Potential

• 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

• Laminar-Flow Airfoils

• High-Lift Airfoil Sections

• Multielement Airfoil Sections for Generating High Lift

• High-Lift Military Airfoils

7. Incompressible Flow 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

• Unmanned Air Vehicle Wings

8. Dynamics of a Compressible Flow Field

• Thermodynamic Concepts

• Adiabatic Flow in a Variable-Area Streamtube

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Tags: John J Bertin, Russell M Cummings, Aerodynamics, Engineers