目次

1.Introduction 1.1 Design Features 1.2 Different Materials in Column Buckling 1.3 Illustrative Examples of Wood, Metal, and Composite Airplanes 1.4 Example Wing Structures 2.Aerodynamic Review 2.1 Airfoils 2.2 Wings 2.3 Bodies 2.4 Undercarriage 2.5 Wing-Body Combination 2.6 Complete-Aircraft Aerodynamics (for a Tail-Aft Monoplane) 2.6.1. Pitching Moment (with non-extended undercarriage) 2.6.2. Pitching Moment (with extended undercarriage) 2.7. Numerical Example 2.7.1. Wing 2.7.2. Tail 2.7.3. Body 2.7.4. Undercarriage 2.7.5. Complete Airplane Lift and Drag Coefficients 2.7.6. Complete Airplane Moment Characteristics 2.8. A Final Comment 3.Propeller Analysis 3.1 Simple Blade-Element Analysis 3.2 Actuator-Disk Momentum Theory 3.3 Extensions to the Simple Blade-Element Analysis 3.4 Method of Calculation. 3.5 Numerical Example 3.6 Propeller Airfoils 3.7 Matlab Program 4.Flying Wings (or Tailless Airplanes) 4.1 “Flying Planks” 4.2 Swept Flying Wings 4.3 Paragliders 4.4 Rogallo-Type Hang Gliders 4.5 Span-Loader Flying Wings 4.6 A Canadian Flying-Wing Glider 4.7 An Approximate Method for Estimating the Aerodynamic Characteristics of Wings with Variable Twist, Taper and Sweep 4.7.1.Example 1, Straight-Tapered Linearly-Twisted Wing. 4.7.2.Example 2, Double-Swept and Double-Tapered Wing 4.7.3.Matlab Computer Program 4.8.“Delta” Tailless Aircraft 4.9.Final Observations 5.Canard Airplanes and Biplanes 5.1 Canard Airplanes 5.1.1. An Approximate Method for Estimating the Aerodynamic 5.1.2. Characteristics of Canard Airplanes 5.1.3. Example, Canard Glider 5.2. Biplanes 5.2.1. An Approximate Method for Estimating the Aerodynamic 5.2.2. Characteristics of Biplanes with Wings of Equal Spans and Areas 5.2.3. Example, “Slow SHARP” Biplane 5.2.4. Further Considerations of Biplane Analysis 5.2.5. Example, Biplane Glider 5.2.6. Final Biplane Comment 6.Flight Dynamics 6.1. Introduction 6.2. Aircraft Longitudinal Small-Perturbation Dynamic Equations 6.2.1 Non-Dimensional Form of the Equations 6.2.2. Estimation of the Longitudinal Stability Derivatives 6.2.3. Longitudinal Numerical Example (“Scholar” Tail-Aft Monoplane) 6.3. Aircraft Lateral Small-Perturbation Dynamic Equations 6.3.1. Non-Dimensional Form of the Equations. 6.3.2. Estimation of the Lateral Stability Derivatives 6.3.3. Example Lateral Stability Derivatives for the “Scholar” Tail- 6.3.4. Aft Monoplane 6.4. Radii-of-Gyration Values for Representative Airplanes 6.5. Definitions of Stability 6.6. Longitudinal Dynamic Stability 6.6.1. Numerical Example 6.6.2. Comments on alpha and theta 6.6.3. Flight Paths 6.6.4. Approximate Equations 6.6.5. Roots-Locus Plots 6.7. Lateral Dynamic Stability 6.7.1. Flight Paths 6.7.2. Approximate Equations 6.7.3. Roots-Locus Plots 6.7.4. Stability-Boundary Plot 6.8. Addendum 7.Performance 7.1. Glide Tests 7.2. Equilibrium Flight 7.3. Trim State 7.4. Full Solution 7.5. Performance Parameters 7.3. Takeoff Run 7.4. Final Comments 8.Balloons and Airships 8.1. Free Balloons 8.2. The Physics of Buoyancy 8.3. Tethered Balloons 8.4. Airships 8.5. Aerodynamics of Finned Axisymmetric Bodies 8.6. A Method for Calculating the Longitudinal Static Aerodynamic Coefficients 8.6.1. Example 1: Small Aerostat 8.6.2. Example 2: Airship ZRS-4 “Akron” 5.98m Wind-Tunnel Model 8.6.3. Example 3: “Wingfoot 2” Airship (Zeppelin LZ N07) 8.6.4. Example 4: TCOM CBV-71 Aerostat 8.7. Aerodynamic Corrections for Inflated Fins 8.6. Additional Observations about Aerostats 8.7. Lateral Force and Yawing Moment Calculation 8.8. Numerical Example 8.9. Airship Aerodynamic Mystery 8.10. Matlab Program. Appendix A: Multhropp Body-Moment Equation Appendix B: Alternative Swept-Wing Analysis Appendix C: Rigid-Body Equations of Motion Appendix D: Apparent-Mass Effects Appendix E: Lift of Finite Wings Due to Oscillatory Plunging Acceleration