Flight Theory and Aerodynamics

FLIGHT THEORY AND AERODYNAMICS

GET A PILOT'S PERSPECTIVE ON FLIGHT AERODYNAMICS FROM THE MOST UP-TO-DATE EDITION OF A CLASSIC TEXT

The newly revised Fourth Edition of Flight Theory and Aerodynamics delivers a pilot-oriented approach to flight aerodynamics without assuming an engineering background. The book connects the principles of aerodynamics and physics to their practical applications in a flight environment. With content that complies with FAA rules and regulations, readers will learn about atmosphere, altitude, airspeed, lift, drag, applications for jet and propeller aircraft, stability controls, takeoff, landing, and other maneuvers.

The latest edition of Flight Theory and Aerodynamics takes the classic textbook first developed by Charles Dole and James Lewis in a more modern direction and includes learning objectives, real world vignettes, and key idea summaries in each chapter to aid in learning and retention. Readers will also benefit from the accompanying online materials, like a test bank, solutions manual, and FAA regulatory references.

Updated graphics included throughout the book correlate to current government agency standards. The book also includes:

• A thorough introduction to basic concepts in physics and mechanics, aerodynamic terms and definitions, and the primary and secondary flight control systems of flown aircraft
• An exploration of atmosphere, altitude, and airspeed measurement, with an increased focus on practical applications
• Practical discussions of structures, airfoils, and aerodynamics, including flight control systems and their characteristics
• In-depth examinations of jet aircraft fundamentals, including material on aircraft weight, atmospheric conditions, and runway environments
• New step-by-step examples of how to apply math equations to real-world situations

Perfect for students and instructors in aviation programs such as pilot programs, aviation management, and air traffic control, Flight Theory and Aerodynamics will also appeal to professional pilots, dispatchers, mechanics, and aviation managers seeking a one-stop resource explaining the aerodynamics of flight from the pilot's perspective.

Auteur

JOSEPH R. BADICK is an Adjunct Faculty Member with Embry-Riddle Aeronautical University, now retired from Guilford Technical Community College. He has over 30 years of experience as an Aeronautical Engineer Duty Officer in the U.S. Navy and over forty years of flight experience in both single and multi-engine land/seaplane aircraft, with an airline transport certificate.

BRIAN A. JOHNSON is an Adjunct Faculty Member in the Aeronautical Science Department of Embry-Riddle Aeronautical University. Additionally, he is a former regional airline and corporate pilot who holds an airline transport pilot certificate with a multi-engine rating.

Texte du rabat

FLIGHT THEORY AND AERODYNAMICS GET A PILOT'S PERSPECTIVE ON FLIGHT AERODYNAMICS FROM THE MOST UP-TO-DATE EDITION OF A CLASSIC TEXT The newly revised Fourth Edition of Flight Theory and Aerodynamics delivers a pilot-oriented approach to flight aerodynamics without assuming an engineering background. The book connects the principles of aerodynamics and physics to their practical applications in a flight environment. With content that complies with FAA rules and regulations, readers will learn about atmosphere, altitude, airspeed, lift, drag, applications for jet and propeller aircraft, stability controls, takeoff, landing, and other maneuvers. The latest edition of Flight Theory and Aerodynamics takes the classic textbook first developed by Charles Dole and James Lewis in a more modern direction and includes learning objectives, real world vignettes, and key idea summaries in each chapter to aid in learning and retention. Readers will also benefit from the accompanying online materials, like a test bank, solutions manual, and FAA regulatory references. Updated graphics included throughout the book correlate to current government agency standards. The book also includes: A thorough introduction to basic concepts in physics and mechanics, aerodynamic terms and definitions, and the primary and secondary flight control systems of flown aircraft An exploration of atmosphere, altitude, and airspeed measurement, with an increased focus on practical applications Practical discussions of structures, airfoils, and aerodynamics, including flight control systems and their characteristics In-depth examinations of jet aircraft fundamentals, including material on aircraft weight, atmospheric conditions, and runway environments * New step-by-step examples of how to apply math equations to real-world situations Perfect for students and instructors in aviation programs such as pilot programs, aviation management, and air traffic control, Flight Theory and Aerodynamics will also appeal to professional pilots, dispatchers, mechanics, and aviation managers seeking a one-stop resource explaining the aerodynamics of flight from the pilot's perspective.

Contenu

Preface xi

About the Authors xiii

About the Companion Website xv

1 Introduction to the Flight Environment 1

Chapter Objectives 1

Introduction 2

Basic Quantities 2

Forces 3

Mass 4

Scalar and Vector Quantities 5

Moments 7

Equilibrium Conditions 8

Newton's Laws of Motion 8

Linear Motion 9

Rotational Motion 11

Energy and Work 11

Power 12

Friction 13

Symbols 14

Key Terms 15

Problems 16

2 Atmosphere, Altitude, and Airspeed Measurement 19

Chapter Objectives 19

Properties of the Atmosphere 19

ICAO Standard Atmosphere 24

Altitude Measurement 24

Continuity Equation 29

Bernoulli's Equation 30

Airspeed Measurement 31

Symbols 38

Key Terms 39

Problems 40

3 Structures, Airfoils, and Aerodynamic Forces 43

Chapter Objectives 43

Aircraft Structures 43

Airfoils 52

Development of Forces on Airfoils 58

Aerodynamic Force 59

Aerodynamic Pitching Moments 61

Aerodynamic Center 63

Accident Brief: Air Midwest Flight 5481 63

Symbols 64

Key Terms 64

Problems 65

4 Lift 69

Chapter Objectives 69

Introduction to Lift 69

Angle of Attack 70

Boundary Layer Theory 71

Reynolds Number 74

Adverse Pressure Gradient 76

Airflow Separation 77

Stall 78

Aerodynamic Force Equations 79

Lift Equation 80

Airfoil Lift Characteristics 84

High Coefficient of Lift Devices 85

Effect of Ice and Frost 89

Lift During Flight Maneuvers 90

Symbols 93

Key Terms 93

Problems 93

5 Drag 97

Chapter Objectives 97

Induced Drag 98

Ground Effect 105

Laminar Flow Airfoils 109

Parasite Drag 110

Drag Equation 114

Total Drag 115

Lift-to-Drag Ratio 117

Drag Reduction 119

Symbols 121

Key Terms 122

Problems 122

6 Jet Aircraft Performance 125

Chapter Objectives 125

Thrust-Producing Aircraft 126

Thrust-Required Curve 129

Principles of Propulsion 130

Thrust-Available Turbojet Aircraft 132

Specific Fuel Consumption 133

Fuel Flow 136

Thrust-Available/Thrust-Required Curves 137

Items of Aircraft Performance 139

Variations in the Thrust-Required Curve 146

Symbols 156

Key Terms 157

Problems 157

7 Propeller Aircraft Performance 161

Chapter Objectives 161

Power Available 162

Principles of Propulsion 166

Power-Required Curves 169

Items of Aircraft Performance 175

Variations in the Power-Required Curve 183

Symbols 193

Key Terms 194

Problems 194

8 Takeoff Performance 199

Chapter Objectives 199

Normal Takeoff 201

Improper Liftoff 206

Rejected Takeoffs 207

Initial Climb 213

Linear Motion 215

Factors Affecting Takeoff Performance 218

Symbols 224

Key Terms 224

Problems 225

9 Landing Performance 229

Chapter Objectives 229

Prelanding Performance 231

Nor…