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Flight Theory and Aerodynamics: A Practical Guide for Operational Safety 4th edition [Kõva köide]

(Embry-Riddle Aeronautical University; Guilford Technical Community College), (Embry-Riddle Aeronautical University)
  • Formaat: Hardback, 480 pages, kõrgus x laius x paksus: 239x193x36 mm, kaal: 953 g
  • Ilmumisaeg: 14-Jan-2022
  • Kirjastus: Wiley-Interscience
  • ISBN-10: 1119772397
  • ISBN-13: 9781119772392
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  • Formaat: Hardback, 480 pages, kõrgus x laius x paksus: 239x193x36 mm, kaal: 953 g
  • Ilmumisaeg: 14-Jan-2022
  • Kirjastus: Wiley-Interscience
  • ISBN-10: 1119772397
  • ISBN-13: 9781119772392
Teised raamatud teemal:
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 propelleor 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.

Preface xi
About the Authors xiii
About the Companion Website xv
1 Introduction to the Flight Environment
1(18)
Chapter Objectives
1(1)
Introduction
2(1)
Basic Quantities
2(1)
Forces
3(1)
Mass
4(1)
Scalar and Vector Quantities
5(2)
Moments
7(1)
Equilibrium Conditions
8(1)
Newton's Laws of Motion
8(1)
Linear Motion
9(2)
Rotational Motion
11(1)
Energy and Work
11(1)
Power
12(1)
Friction
13(1)
Symbols
14(1)
Key Terms
15(1)
Problems
16(3)
2 Atmosphere, Altitude, and Airspeed Measurement
19(24)
Chapter Objectives
19(1)
Properties of the Atmosphere
19(5)
ICAO Standard Atmosphere
24(1)
Altitude Measurement
24(5)
Continuity Equation
29(1)
Bernoulli's Equation
30(1)
Airspeed Measurement
31(7)
Symbols
38(1)
Key Terms
39(1)
Problems
40(3)
3 Structures, Airfoils, and Aerodynamic Forces
43(26)
Chapter Objectives
43(1)
Aircraft Structures
43(9)
Airfoils
52(6)
Development of Forces on Airfoils
58(1)
Aerodynamic Force
59(2)
Aerodynamic Pitching Moments
61(2)
Aerodynamic Center
63(1)
Accident Brief: Air Midwest Flight 5481
63(1)
Symbols
64(1)
Key Terms
64(1)
Problems
65(4)
4 Lift
69(28)
Chapter Objectives
69(1)
Introduction to Lift
69(1)
Angle of Attack
70(1)
Boundary Layer Theory
71(3)
Reynolds Number
74(2)
Adverse Pressure Gradient
76(1)
Airflow Separation
77(1)
Stall
78(1)
Aerodynamic Force Equations
79(1)
Lift Equation
80(4)
Airfoil Lift Characteristics
84(1)
High Coefficient of Lift Devices
85(4)
Effect of Ice and Frost
89(1)
Lift During Flight Maneuvers
90(3)
Symbols
93(1)
Key Terms
93(1)
Problems
93(4)
5 Drag
97(28)
Chapter Objectives
97(1)
Induced Drag
98(7)
Ground Effect
105(4)
Laminar Flow Airfoils
109(1)
Parasite Drag
110(4)
Drag Equation
114(1)
Total Drag
115(2)
Lift-to-Drag Ratio
117(2)
Drag Reduction
119(2)
Symbols
121(1)
Key Terms
122(1)
Problems
122(3)
6 Jet Aircraft Performance
125(36)
Chapter Objectives
125(1)
Thrust-Producing Aircraft
126(3)
Thrust-Required Curve
129(1)
Principles of Propulsion
130(2)
Thrust-Available Turbojet Aircraft
132(1)
Specific Fuel Consumption
133(3)
Fuel Flow
136(1)
Thrust-Available/Thrust-Required Curves
137(2)
Items of Aircraft Performance
139(7)
Variations in the Thrust-Required Curve
146(10)
Symbols
156(1)
Key Terms
157(1)
Problems
157(4)
7 Propeller Aircraft Performance
161(38)
Chapter Objectives
161(1)
Power Available
162(4)
Principles of Propulsion
166(3)
Power-Required Curves
169(6)
Items of Aircraft Performance
175(8)
Variations in the Power-Required Curve
183(10)
Symbols
193(1)
Key Terms
194(1)
Problems
194(5)
8 Takeoff Performance
199(30)
Chapter Objectives
199(2)
Normal Takeoff
201(5)
Improper Liftoff
206(1)
Rejected Takeoffs
207(6)
Initial Climb
213(2)
Linear Motion
215(3)
Factors Affecting Takeoff Performance
218(6)
Symbols
224(1)
Key Terms
224(1)
Problems
225(4)
9 Landing Performance
229(36)
Chapter Objectives
229(2)
Prelanding Performance
231(7)
Normal Landing
238(6)
Improper Landing Performance
244(3)
Hazards of Hydroplaning
247(3)
Landing Deceleration, Velocity, and Distance
250(5)
Landing Equations
255(5)
Symbols
260(1)
Key Terms
260(1)
Problems
261(4)
10 Slow-Speed Flight
265(30)
Chapter Objectives
265(1)
Region of Reversed Command
266(4)
Stalls
270(8)
Spins
278(5)
Hazards During Slow-Speed Flight - Low-Level Wind Shear
283(2)
Aircraft Performance in Low-Level Wind Shear
285(4)
Hazards During Slow-Speed Flight - Wake Turbulence
289(3)
Key Terms
292(1)
Problems
292(3)
11 Maneuvering Performance
295(24)
Chapter Objectives
295(1)
General Turning Performance
295(2)
Load Factor
297(6)
The V-G Diagram (Flight Envelope)
303(5)
Load Factor and Flight Maneuvers
308(8)
Symbols
316(1)
Key Terms
316(1)
Problems
317(2)
12 Longitudinal Stability and Control
319(32)
Chapter Objectives
319(1)
Definitions
320(2)
Oscillatory Motion
322(1)
Weight and Balance
323(5)
Airplane Reference Axes
328(1)
Static Longitudinal Stability
329(12)
Dynamic Longitudinal Stability
341(1)
Pitching Tendencies in a Stall
342(3)
Longitudinal Control
345(2)
Symbols
347(1)
Key Terms
347(1)
Problems
348(3)
13 Directional and Lateral Stability
351(34)
Chapter Objectives
351(1)
Static Directional Stability
352(7)
Directional Control
359(5)
Multi-Engine Flight Principles
364(4)
Lateral Stability and Control
368(1)
Static Lateral Stability
368(6)
Lateral Control
374(1)
Dynamic Directional and Lateral Coupled Effects
374(6)
Symbols
380(1)
Key Terms
380(1)
Problems
380(5)
14 High-Speed Flight
385(30)
Chapter Objectives
385(1)
The Speed of Sound
386(3)
High-Subsonic Flight
389(1)
Design Features for High-Subsonic Flight
390(5)
Transonic Flight
395(4)
Supersonic Flight
399(12)
Symbols
411(1)
Key Terms
411(1)
Problems
412(3)
15 Rotary-Wing Flight Theory
415(28)
Chapter Objectives
415(2)
Momentum Theory of Lift
417(1)
Airfoil Selection
417(1)
Forces on Rotor System
418(2)
Thrust Development
420(1)
Hovering Flight
420(3)
Ground Effect
423(2)
Rotor Systems
425(1)
Dissymmetry of Lift in Forward Flight
426(3)
High Forward Speed Problems
429(3)
Helicopter Control
432(1)
Helicopter Power-Required Curves
433(2)
Power Settling, Settling with Power, and Vortex Ring State
435(2)
Autorotation
437(3)
Dynamic Rollover
440(1)
Problems
440(3)
Answers to Problems 443(4)
Bibliography 447(4)
Index 451
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.