Johnson / Fittante | Flight Theory and Aerodynamics | Buch | 978-1-394-28229-6 | sack.de

Buch, Englisch, 608 Seiten

Johnson / Fittante

Flight Theory and Aerodynamics

A Practical Guide for Operational Safety
5. Auflage 2026
ISBN: 978-1-394-28229-6
Verlag: John Wiley & Sons Inc

A Practical Guide for Operational Safety

Buch, Englisch, 608 Seiten

ISBN: 978-1-394-28229-6
Verlag: John Wiley & Sons Inc


Comprehensive introduction to aerodynamics applied to different types of modern aircraft, now updated with the latest FAA guidance

Flight Theory and Aerodynamics provides an introduction to aerodynamics using practical application to modern aircraft with step-by-step calculations. This fifth edition streamlines content, notably the chapters on aircraft stability, and incorporates updated FAA guidance and figures from the 2023 Pilot’s Handbook of Aeronautical Knowledge as well as other FAA handbooks.

A balanced application of introductory physics and meteorology in the first five chapters evolves into an introduction to propeller and jet aircraft propulsion and eventually moves into a broad discussion on the application of physics to aircraft takeoff and landing performance. After the introductory material has been presented, principles from earlier in the textbook and prior coursework are correlated and applied to slow flight, aircraft stability, and high-speed flight. A new chapter on Unmanned Aerial Vehicle (UAV) flight theory is included.

The text features extensive instructor resources including detailed PowerPoint slides for each chapter, step-by-step guidance for end of chapter calculations, sample test bank questions for each chapter, and application sections within each chapter that allow the instructor to challenge the student with additional real-world scenarios based on chapter content.

Flight Theory and Aerodynamics includes information on: - Elements of the flight environment, covering forces, mass, scalar and vector quantities, linear and rotational motion, friction, and power
- Atmosphere, altitude, and airspeed measurement, covering properties of the atmosphere, Bernoulli’s equation, and pitot-static system advantages and disadvantages
- Jet aircraft performance, covering principles of propulsion, fuel flow, specific fuel consumption, and thrust-required curves
- Aircraft stability and control, covering oscillatory motion, weight and balance, and airplane reference axes
- Rotary-wing flight theory, airfoil selection, and helicopter control
- UAV flight theory, including UAV design considerations, the aerodynamics of UAV fuselage design, UAV powerplant design, and the future of UAV design and aerodynamics
- End of chapter questions focused on scenario-based learning as applied to the performance analysis of a Diamond DA50 and corresponding chapter material.

In addition to degree-oriented college programs, this latest edition of Flight Theory and Aerodynamics is also an essential resource for pilot training programs ranging from student pilots to flight instructors as well as practicing professionals flying a wide range of aircraft.

Johnson / Fittante Flight Theory and Aerodynamics jetzt bestellen!

Weitere Infos & Material


1 Introduction to the Flight Environment. 15

Introduction. 16

History of Aerodynamics. 16

Basic Quantities. 21

Forces. 22

Mass. 24

Scalar and Vector Quantities. 24

Scalar Addition. 24

Vector Addition. 25

Vector Resolution. 26

Moments. 27

Equilibrium Conditions. 28

Newton’s Laws of Motion. 29

Newton’s First Law. 29

Newton’s Second Law. 29

Newton’s Third Law. 30

Energy and Work. 30

Power. 31

Friction. 32

Introduction to Linear Motion. 33

introduction to Rotational Motion. 35

CHAPTER 1 Symbols. 36

CHAPTER 1 EQUATIONS. 37

CHAPTER 1 KEY TERMS. 37

CHAPTER 1 PROBLEMS. 39

CHAPTER 1 BIBLIOGRAPHY. 42

2 Atmosphere, Altitude, and Airspeed Measurement. 44

PROPERTIES OF THE ATMOSPHERE. 44

Static Pressure. 45

Temperature. 46

Density. 48

Viscosity. 50

ICAO Standard Atmosphere. 50

Altitude Measurement. 51

Indicated Altitude. 51

Calibrated Altitude. 52

True Altitude. 52

Absolute Altitude. 52

Pressure Altitude. 53

Density Altitude. 54

Continuity Equation. 56

Bernoulli's Equation. 57

Airspeed Measurement. 60

Indicated Airspeed. 63

Calibrated Airspeed. 63

Equivalent Airspeed. 64

True Airspeed. 64

Mach. 66

Groundspeed. 67

CHAPTER 2 Symbols. 67

CHAPTER 2 EQUATIONS. 68

CHAPTER 2 KEY TERMS. 69

CHAPTER 2 PROBLEMS. 70

CHAPTER 2 BIBLIOGRAPHY. 74

3 Structures, Airfoils, and Aerodynamic Forces. 75

AIRCRAFT STRUCTURES. 75

Primary Flight Controls. 76

Secondary Flight Controls. 83

AIRFOILS. 89

Airfoil Terminology. 90

Definitions. 90

Geometry Variables of Airfoils. 91

Classification of Airfoils. 93

DEVELOPMENT OF FORCES ON AIRFOILS. 96

Pressure Disturbances on Airfoils. 96

Velocity and Static Pressure Changes about an Airfoil 97

AERODYNAMIC FORCE. 98

Pressure Distribution on a Rotating Cylinder. 98

AERODYNAMIC PITCHING MOMENTS. 99

AERODYNAMIC CENTER. 102

ACCIDENT BRIEF: AIR MIDWEST FLIGHT 5481. 103

CHAPTER 3 SYMBOLS. 104

CHAPTER 3 KEY TERMS. 104

CHAPTER 3 PROBLEMS. 105

CHAPTER 3 BIBLIOGRAPHY. 109

4 Lift. 110

Introduction to Lift. 110

Angle of Attack. 111

Angle of Attack Indicator. 112

Accident Brief: Air France Flight 447. 114

Angle of Attack and Coefficient of Lift. 115

Boundary Layer Theory. 116

Coanda Effect. 119

Reynolds Number. 119

Adverse Pressure Gradient. 121

Airflow Separation. 122

Stall 124

Aerodynamic Force Equations. 126

Lift Equation. 126

Coefficient of Lift and the Lift Equation. 127

Velocity. 129

Lift Formula Summary. 131

Airfoil Lift Characteristics. 132

High Coefficient of Lift Devices. 133

Effect of Ice and Frost. 141

Lift During Flight Maneuvers. 142

Lift During Turns. 143

Lift During Climbs and Descents. 144

Lift and Balloons. 145

CHAPTER 4 Symbols. 147

CHAPTER 4 EQUATIONS. 148

CHAPTER 4 KEY TERMS. 148

CHAPTER 4 PROBLEMS. 149

CHAPTER 4 BIBLIOGRAPHY. 153

5 Drag. 155

Induced Drag. 155

Aspect Ratio. 158

Wingtip Vortices. 160

Infinite Wing. 161

Finite Wing. 162

Induced Drag Summary. 164

Ground Effect. 165

Airflow Alteration Around the Wing. 166

Pitching Moments. 167

Pitot–Static Influence. 168

Ground Effect Summary. 168

Parasite Drag. 170

Skin Friction Drag. 170

Laminar Flow Airfoils. 171

Form Drag. 174

Interference Drag. 175

Leakage Drag. 176

Parasite Drag Summary. 176

Drag Equation. 177

Induced and Parasite Drag Calculations. 178

Total Drag. 179

Lift-to-Drag Ratio. 181

(L/D)max Summary. 185

Drag Reduction. 186

Winglet Design. 186

Winglet Application. 189

CHAPTER 5 Symbols. 190

CHAPTER 5 EQUATIONS. 191

CHAPTER 5 KEY TERMS. 191

CHAPTER 5 PROBLEMS. 193

CHAPTER 5 BIBLIOGRAPHY. 197

6 Jet Aircraft Performance. 199

Thrust-Producing Aircraft. 200

Turbine Engine Operation. 201

Thrust-Required Curve. 203

Principles of Propulsion. 204

Thrust-Available Turbojet Aircraft. 206

Thrust Variation and rpm. 206

Specific Fuel Consumption. 209

Fuel Flow. 211

Thrust-Available/Thrust-Required Curves. 211

Items of Aircraft Performance. 212

Straight and Level Flight. 212

Climb Performance. 213

Angle of Climb. 214

Rate of Climb. 215

Endurance. 218

Specific Range. 219

Wind Effect on Specific Range. 220

Total Range. 220

Variations in the Thrust-Required Curve. 221

Weight Changes. 222

Configuration Changes. 226

Altitude Changes. 228

Cruise–Climb Flight. 230

Afterburners and Vectored Thrust. 231

Jet Performance Summary. 232

CHAPTER 6 Symbols. 233

CHAPTER 6 EQUATIONS. 234

CHAPTER 6 KEY TERMS. 235

CHAPTER 6 PROBLEMS. 235

CHAPTER 6 BIBLIOGRAPHY. 239

7 Propeller Aircraft Performance. 241

POWER AVAILABLE. 242

Basic Propeller Principles. 243

Fixed-Pitch Propeller. 245

Constant-Speed Propeller. 246

PRINCIPLES OF PROPULSION. 248

POWER-REQUIRED CURVES. 251

Power Available Versus Velocity. 253

Variations with Power and Altitude. 255

ITEMS OF AIRCRAFT PERFORMANCE. 258

Straight and Level Flight. 258

Climb Performance. 258

Angle of Climb. 259

Rate of Climb. 261

Endurance. 263

Specific Range. 265

Wind Effect on Specific Range. 265

VARIATIONS IN THE POWER-REQUIRED CURVE. 266

Weight Changes. 266

Configuration Change. 270

Altitude Changes. 272

Propeller Performance Summary. 276

CHAPTER 7 SYMBOLS. 277

CHAPTER 7 EQUATIONS. 278

CHAPTER 7 KEY TERMS. 278

CHAPTER 7 PROBLEMS. 279

Chapter 7 Bibliography. 286

8 Takeoff Performance. 287

Normal Takeoff. 290

Crosswind Takeoff. 291

Performance Takeoffs. 293

Water Takeoffs. 295

Performance Speeds – Normal Takeoff. 296

Improper Liftoff. 297

Premature Takeoff in Ground Effect. 297

Dangers of Over-rotation. 298

Rejected Takeoffs. 298

RTO V-Speeds and Definitions. 299

Declared Distances. 302

Single-Engine Airplane. 303

Multi-Engine Airplane. 304

Rejected Takeoff Aerodynamics. 306

Initial Climb. 310

Linear Motion. 313

Factors Affecting Takeoff Performance. 316

Weight Change. 316

Altitude. 318

Wind. 319

Runway Surface. 322

Runway Slope. 323

CHAPTER 8 Symbols. 324

CHAPTER 8 EQUATIONS. 324

CHAPTER 8 kEY TERMS. 325

CHAPTER 8 PROBLEMS. 326

Chapter 8 Bibliography. 331

9 Landing Performance. 333

PRELANDING PERFORMANCE. 335

Gliding Flight. 336

The Landing Approach. 338

Stabilized Approaches. 339

Approach Glide Paths. 340

NORMAL LANDING. 345

Crosswind Landing. 345

Performance Landings. 347

IMPROPER LANDING PERFORMANCE. 349

Improper Round Out. 349

Bouncing and Ballooning. 350

Porpoising. 351

Rejected Landings (Go-arounds). 352

HAZARDS OF HYDROPLANING. 353

Dynamic Hydroplaning. 353

Viscous Hydroplaning. 356

Reverted Rubber Hydroplaning. 356

LANDING DECELERATION, VELOCITY, AND DISTANCE. 356

Forces on the Aircraft During Landing. 356

Braking Techniques. 361

Thrust Reversers. 361

LANDING EQUATIONS. 363

General Equation. 363

Effect of Weight Change. 364

Effect of Altitude. 365

Effect of Wind. 366

LANDING ENVIRONMENT. 369

Accident Brief: Southwest Airlines (SWA) Flight 1248. 369

Runway Surface. 370

Runway Slope. 373

CHAPTER 9 SYMBOLS. 373

CHAPTER 9 EQUATIONS. 373

CHAPTER 9 KEY TERMS. 374

CHAPTER 9 PROBLEMS. 375

Chapter 9 Bibliography. 380

10 Slow-Speed Flight. 382

Region of Reversed Command. 383

Thrust producers. 384

Power producers. 387

Stalls. 388

Stall Patterns. 388

Stall Warning Devices. 391

Stall Recovery. 391

Power-Off Stall 393

Power-On Stall 394

Accelerated Stall 395

Cross-Control Stall 396

Uncoordinated Flight. 397

Spins. 399

Spin Warning. 399

Aerodynamic Characteristics of a Spin. 401

Impact of Weight and Balance During a Spin. 404

Hazards During Slow-Speed Flight – Low-Level Wind Shear. 405

Aircraft Performance in Low-Level Wind Shear. 407

During Takeoff and Departure. 407

During Approach to a Landing. 409

Vertical Shear Level 410

Crosswind Burst Response. 412

Heavy Rain. 412

Hazards During Slow-Speed Flight – Turbulence. 413

Turbulence Effects. 413

Wake Turbulence. 413

Mechanical Turbulence. 416

Convection and Mountain Wave Turbulence. 417

Chapter 10 EQUATIONS. 419

Chapter 10 Key Terms. 419

Chapter 10 Problems. 420

Chapter 10 Bibliography. 424

11 Maneuvering Performance. 426

General Turning Performance. 426

Forces in Turns. 429

Load Factor. 430

Load Factors on an Aircraft in a Coordinated Turn. 432

Effect of a Coordinated Banked Turn on Stall Speed. 433

The V–G Diagram (Flight Envelope). 436

Maneuver Speed and Limit Load Factor. 440

Load Factor and Flight Maneuvers. 443

Radius of Turn. 444

Rate of Turn. 448

Energy Management. 451

The Airplane as an Energy System. 452

Energy System Control 453

Application of the Energy System. 455

CHAPTER 11 Symbols. 458

CHAPTER 11 EQUATIONS. 458

CHAPTER 11 KEY TERMS. 459

CHAPTER 11 PROBLEMS. 460

Chapter 11 Bibliography. 464

12 Longitudinal Stability and Control 465

Definitions. 466

Equilibrium. 466

Static Stability. 466

Dynamic Stability. 467

Oscillatory Motion. 468

Weight and Balance. 469

Weight and Balance Theory. 470

Mean Aerodynamic Chord. 472

Effect of Weight on Flight Performance. 473

Effect of Weight on Load Distribution. 474

Airplane Reference Axes. 476

Static Longitudinal Stability. 479

The Pitching Moment Equation. 479

Graphic Representation of Static Longitudinal Stability. 480

Contribution of Aircraft Components to Pitch Stability. 481

Static Margin and Neutral Point. 490

Stick-Fixed Versus Stick-Free Stability. 492

Accident Brief: B-1A Static Margin Test. 492

Dynamic Longitudinal Stability. 494

Pitching Tendencies in a Stall 496

Low-Tailed Aircraft. 496

T-Tail Aircraft. 497

Explanation of Nose-Up Pitch Following Stall in Swept-Wing Aircraft. 498

Longitudinal Control 500

CHAPTER 12 Symbols. 501

CHAPTER 12 EQUATIONS. 502

CHAPTER 12 KEY TERMS. 502

CHAPTER 12 PROBLEMS. 503

Chapter 12 Bibliography. 507

13 Directional and Lateral Stability. 509

Static Directional Stability. 509

The Yawing Moment Equation. 511

Graphic Representation of Static Directional Stability. 511

Contribution of Aircraft Components to Yaw Stability. 512

Directional Control 517

Slipstream Rotation. 517

Crosswind Takeoff and Landing. 518

Asymmetrical Loading/Thrust. 518

Intentional Slips. 522

Multi-Engine Flight Principles. 524

Introduction to Single-Engine Flight. 525

Flight Principles with One Engine Inoperative. 526

VMC Considerations. 528

Lateral Stability and Control 531

Static Lateral Stability. 531

The Rolling Moment Equation. 533

Graphic Representation of Static Lateral Stability. 533

Contributions of Aircraft Components to Roll Stability. 534

Lateral Control 539

Dynamic Directional and Lateral Coupled Effects. 539

Roll Due to Yawing. 539

Adverse Yaw. 540

Types of Motion Resulting from Coupled Effects. 543

CHAPTER 13 Symbols. 546

CHAPTER 13 EQUATIONS. 547

CHAPTER 13 KEY TERMS. 547

CHAPTER 13 PROBLEMS. 548

Chapter 13 Bibliography. 551

14 High-Speed Flight. 552

THE SPEED OF SOUND. 552

Coffin Corner (Q Corner). 555

HIGH-SUBSONIC FLIGHT. 556

Normal Shock Wave Formation on Wings. 556

DESIGN FEATURES FOR HIGH-SUBSONIC FLIGHT. 557

Thin Airfoil Sections. 558

High-Speed Subsonic Airfoils. 558

Sweepback. 559

Vortex Generators. 561

High-Speed Subsonic Control Surfaces. 561

Flight Control Augmentation Systems. 563

TRANSONIC FLIGHT. 565

Wave Drag and Force Divergence. 565

Mach Tuck. 567

High-Speed Mach Buffet. 569

Control Surface Buzz and Flutter. 569

SUPERSONIC FLIGHT. 570

Oblique Shock Waves. 571

Expansion Waves. 572

Aerodynamic Forces in Supersonic Flight. 574

Supersonic Airfoils. 574

Wing Planform. 576

Area Rule Drag Reduction. 578

Control Effectiveness. 579

Supersonic Engine Inlets. 581

Aerodynamic Heating. 584

Computational Fluid Dynamics and Computer-Aided Design. 586

Low Boom Flight Development. 588

chapter 14 SYMBOLS. 591

chapter 14 EQUATIONS. 591

chapter 14 KEY TERMS. 591

chapter 14 pROBLEMS. 592

Chapter 14 Bibliography. 595

15 Rotary-Wing Flight Theory. 597

MOMENTUM THEORY OF LIFT. 599

AIRFOIL SELECTION. 599

FORCES ON ROTOR SYSTEM. 600

THRUST DEVELOPMENT. 603

HOVERING FLIGHT. 603

Hovering Blade Velocity. 605

Blade Twist. 605

GROUND EFFECT. 605

Torque. 606

ROTOR SYSTEMS. 608

Rigid Rotor. 608

Semirigid Rotor (Seesaw or Teetering Hinge). 609

Fully Articulated Rotor. 609

DISSYMMETRY OF LIFT IN FORWARD FLIGHT. 610

Blade Flapping. 611

Blade Lead and Lag. 612

HIGH FORWARD SPEED PROBLEMS. 613

Advancing Blade Compressibility. 613

Retreating Blade Stall 614

Gyroscopic Precession. 615

HELICOPTER CONTROL. 615

Rotor Head Control 616

Control of the Path. 617

HELICOPTER POWER-REQUIRED CURVES. 617

Translational Lift. 618

POWER SETTLING, SETTLING WITH POWER, AND VORTEX RING STATE. 619

AUTOROTATION. 622

DYNAMIC ROLLOVER. 624

CHAPTER 15 PROBLEMS. 625

CHAPTER 15 BIBLIOGRAPHY. 627

16 Unmanned Aerial Vehicle Flight Theory. 628

UAV Categorization. 630

UAV Design. 630

Aerodynamics of UAV Fuselage Design. 632

UAV Powerplant Design. 634

The Future of UAV Design and Aerodynamics. 640

CHAPTER 16 KEY TERMS. 644

CHAPTER 16 BIBLIOGRAPHY. 644


Brian A. Johnson is a former regional airline pilot, corporate pilot, and part 141 chief ground instructor. He holds an ATP with an MEL rating, commercial pilot SEL/SES and sUAS, and currently serves as an active gold seal CFII/MEI, full-time company pilot, and a regional FAASTeam representative.

Philip R. Fittante is a retired US Air Force Lieutenant Colonel with flight time in over 40 types of aircraft. He served as the Chief Developmental Test Pilot for the B-1B and B-2 bombers, possessing nearly 30 years of experience as an Air Force test pilot and Navy civilian test pilot and engineer.



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