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Badick Joseph Robert - Flight theory and aerodynamics: a practical guide for operational safety

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Badick Joseph Robert Flight theory and aerodynamics: a practical guide for operational safety

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The pilots guide to aeronautics and the complex forces of flight Flight Theory and Aerodynamics is the essential pilots guide to the physics of flight, designed specifically for those with limited engineering experience. From the basics of forces and vectors to craft-specific applications, this book explains the mechanics behind the pilots everyday operational tasks. The discussion focuses on the concepts themselves, using only enough algebra and trigonometry to illustrate key concepts without getting bogged down in complex calculations, and then delves into the specific applications for jets, propeller crafts, and helicopters. This updated third edition includes new chapters on Flight Environment, Aircraft Structures, and UAS-UAV Flight Theory, with updated craft examples, component photos, and diagrams throughout. FAA-aligned questions and regulatory references help reinforce important concepts, and additional worked problems provide clarification on complex topics. Modern flight control systems are becoming more complex and more varied between aircrafts, making it essential for pilots to understand the aerodynamics of flight before they ever step into a cockpit. This book provides clear explanations and flight-specific examples of the physics every pilot must know. Review the basic physics of flight Understand the applications to specific types of aircraft Learn why takeoff and landing entail special considerations Examine the force concepts behind stability and control As a pilot, your job is to balance the effects of design, weight, load factors, and gravity during flight maneuvers, stalls, high- or low-speed flight, takeoff and landing, and more. As aircraft grow more complex and the controls become more involved, an intuitive grasp of the physics of flight is your most valuable tool for operational safety. Flight Theory and Aerodynamics is the essential resource every pilot needs for a clear understanding of the forces they control--

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Table of Contents List of Illustrations Chapter 1 Introduction Chapter 2 - photo 1

Table of Contents
List of Illustrations
  1. Chapter 1: Introduction
  2. Chapter 2: Atmosphere, Altitude, and Airspeed Measurement
  3. Chapter 3: Structures, Airfoils, and Aerodynamic Forces
  4. Chapter 4: Lift
  5. Chapter 5: Drag
  6. Chapter 6: Jet Aircraft Basic Performance
  7. Chapter 7: Jet Aircraft Applied Performance
  8. Chapter 8: Propeller Aircraft: Basic Performance
  9. Chapter 9: Propeller Aircraft: Applied Performance
  10. Chapter 10: Takeoff Performance
  11. Chapter 11: Landing Performance
  12. Chapter 12: SlowSpeed Flight
  13. Chapter 13: Maneuvering Performance
  14. Chapter 14: Longitudinal Stability and Control
  15. Chapter 15: Directional and Lateral Stability and Control
  16. Chapter 16: HighSpeed Flight
  17. Chapter 17: RotaryWing Flight Theory
List of Tables
  1. Chapter 2: Atmosphere, Altitude, and Airspeed Measurement
  2. Chapter 13: Maneuvering Performance
Guide
Pages
Answers to Problems
CHAPTER 1

1. m = 500 slugs; 2. a = 12 fps2; 3. Drag = 282 lb, Lift = 102.6 lb; 4. Tan = 0.75, Distance = 5 mi; 5. s = 8 ft, F = 30 lb; 6. Time = 16.7 sec; 7. Takeoff roll = 1667 ft; 8. a = 5 fps2; 9. V1 = 450 fps; 10. PE = 80 106 ftlb, KE = 10 106 ftlb, TE = 90 106 ftlb; 11. HP = 5000 hp; 12. Flight theory and aerodynamics a practical guide for operational safety - image 2

CHAPTER 2

1. c; 2. c; 3. a; 4. a; 5. d; 6. d; 7. c; 8. b; 9. a; 10. b; 11. d = 0.929, PA = 2000 ft, q = 1.078, s = 0.8618, DA = 5000 ft; 12. H = 2062.8 psf, P2 = 1931 psf, q2 = 131 psf, Picture 3, Picture 4, Picture 5; 13. q = 116.8 psf; 14. EAS = 337.5 knots; 15. TAS = 498 knots

CHAPTER 3

1. d; 2. c; 3. d; 4. d; 5. c; 6. e; 7. d; 8. d; 9. b; 10. d

CHAPTER 4

1. a; 2. c; 3. a; 4. c; 5. d; 6. d; 7. c; 8. b; 9. d; 10. a. combination, b. energy add, c. combination, d. camber chg; 11. AOA = 4; 12. Flight theory and aerodynamics a practical guide for operational safety - image 6; 13. Flight theory and aerodynamics a practical guide for operational safety - image 7; 14. Flight theory and aerodynamics a practical guide for operational safety - image 8

CHAPTER 5

1. d; 2. c; 3. d; 4. d; 5. b; 6. d; 7. d; 8. c; 9. b; 10. b; 11. Flight theory and aerodynamics a practical guide for operational safety - image 9; 12. V = 172 knots; 13. Flight theory and aerodynamics a practical guide for operational safety - image 10

V2(V2/V1)Dp(V1/V2)2DiDt
1250.5302701.899631233
1500.7633891.316691058
1721.05101.05101020
2001.356900.743771067
3003.0415620.331681720
4005.4227660.184942860
CHAPTER 6

1. d; 2. d; 3. a; 4. a; 5. a; 6. a; 7. d; 8. c; 9. c; 10. b; 11. T = 3000 lb, Efficiency = 77%; 12. Flight theory and aerodynamics a practical guide for operational safety - image 11, T = 4100 lb, FF0 = 6150 lb/hr; 13. Flight theory and aerodynamics a practical guide for operational safety - image 12; 14. a. 500 knots, b. 240 knots, c. 0.327 (19), d. 10,940 fpm, e. 240 knots, f. 300 knots, g. 350 knots

CHAPTER 7

1. d; 2. c; 3. a; 4. b; 5. d; 6. a; 7. d; 8. c; 9. b; 10. d; 11. Flight theory and aerodynamics a practical guide for operational safety - image 13, Flight theory and aerodynamics a practical guide for operational safety - image 14; 12. Flight theory and aerodynamics a practical guide for operational safety - image 15, Flight theory and aerodynamics a practical guide for operational safety - image 16; 13. Flight theory and aerodynamics a practical guide for operational safety - image 17, SR improvement in Problem 13 = 14.154%, SR improvement in Problem 12 = 27.6%, conclusion: reduce throttle as fuel is burned; 14. SR0 = 0.2973, SR20 = 0.4108, SR improvement = 38%

CHAPTER 8

1. a; 2. d; 3. c; 4. b; 5. d; 6. b; 7. b; 8. d; 9. c; 10. b; 11. 474 HP, 488 HP, 540 HP, 657 HP, 1588 HP, 3520 HP; 12. a. 340 knots, b. 0.542 (32.8), c. 0.37 (21.7), d. 4125 fpm, e. 4950 fpm, f. 100 knots, g. 140 knots, h. 160 knots

CHAPTER 9

1. c; 2. a; 3. b; 4. c; 5. c; 6. c; 7. c; 8. b; 9. b; 10. a; 11. Flight theory and aerodynamics a practical guide for operational safety - image 18, Flight theory and aerodynamics a practical guide for operational safety - image 19; 12. Flight theory and aerodynamics a practical guide for operational safety - image 20, Flight theory and aerodynamics a practical guide for operational safety - image 21; 13. Flight theory and aerodynamics a practical guide for operational safety - image 22, Improvement = 18.7%, Improvement in Problem 12 = 53.5%; conclusion: reduce throttle as fuel is burned; 14. SR0 = SR = 0.58 nmi/lb; conclusion: no change in SR with altitude (considering airframe only)

CHAPTER 10

1. d; 2. c; 3. c; 4. d; 5. a; 6. d; 7. d; 8. a; 9. a; 10. Picture 23; 11. V = 126.5 fps (75 knots); 12. S = 2576 ft; 13. S = 5796 ft; 14. S = 2087 ft; 15. S = 4025 ft

CHAPTER 11

1. d; 2. b; 3. d; 4. d; 5. d; 6. a; 7. a; 8. c; 9. a; 10. a; 11. Picture 24; 12.

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