General aviation aircraft design : applied methods and procedures /


Snorri Gudmundsson.
Bok Engelsk 2022 · Electronic books.

Omfang
1 online resource (1146 pages)
Utgave
Second edition.
Opplysninger
Intro -- General Aviation Aircraft Design: Applied Methods and Procedures -- Copyright -- Dedication -- Contents -- Preface to the 1st Edition -- Preface to the 2nd Edition -- Acknowledgments for the 1st Edition -- Acknowledgments for the 2nd Edition -- Disclaimer -- Helpful Notes -- Helpful Websites for the Aircraft Designer -- The Greek Alphabet -- Prefixes for SI Units -- Prefixes for SI Units -- A Note About Format -- A Note About Mass and Force -- List of Abbreviations and Common Terms -- List of Variables -- Chapter 1: The Aircraft Design Process -- 1.1. Introduction -- 1.1.1. The Contents of This Chapter -- 1.1.2. Why Do We Need an Aircraft Design Process? -- 1.2. General Process of Aircraft Design and Development -- 1.2.1. Common Descriptions of the Design Process -- 1.2.2. Fundamental Phases of the Aircraft Design Process -- 1.2.3. Concepts of Importance to the Aircraft Design Process -- 1.2.4. Development Timeline for Typical GA Aircraft -- 1.3. Introduction to Aviation Regulations and Certification -- 1.3.1. Aviation Regulations That Apply to GA Aircraft -- 1.3.2. Important Regulatory Concepts -- 1.4. How to Design a New Aircraft -- 1.4.1. Conceptual Design Algorithm for a General Aviation Aircraft -- 1.4.2. Implementation of the Conceptual Design Algorithm -- 1.5. Elements of Project Engineering -- 1.5.1. Project Plan -- 1.5.2. Team Leadership -- 1.5.3. Task Management and the Task Matrix -- 1.5.4. Gantt Diagrams -- 1.5.5. PERT Charts -- 1.5.6. Fishbone Diagram for Preliminary Airplane Design -- 1.5.7. Documentation Standards and Drawing Organizing -- 1.5.8. Quality Function Deployment and a House of Quality -- 1.6. Presenting the Design Project -- References -- Chapter 2: Aircraft Cost Analysis -- 2.1. Introduction -- 2.1.1. The Content of This Chapter -- 2.1.2. A Review of the State of the General Aviation Industry.. - 2.1.3. The Basics of Development Cost Analysis -- 2.1.4. Important Concepts in Air Transport Economics -- 2.2. The Estimation of Project Development Costs -- 2.2.1. Development Cost of a GA Aircraft -- 2.2.2. Development Cost of a Business Aircraft -- 2.2.3. A Word About the Accuracy of the Eastlake Model -- 2.3. Estimating Aircraft Operational Costs -- 2.3.1. Direct Operational Cost of a GA Aircraft -- 2.3.2. Direct Operational Cost of a Business Aircraft -- 2.3.3. A Word About Aircraft Operational Cost -- Exercises -- References -- Chapter 3: Initial Sizing -- 3.1. Introduction -- 3.1.1. The Content of This Chapter -- 3.1.2. Fundamental Concepts -- 3.2. Constraint Analysis -- 3.2.1. General Methodology -- 3.2.2. Methodology to Accommodate Normally Aspirated Piston Engines -- 3.2.3. Additional Helpful Tools for Initial Sizing -- 3.3. Introduction to Trade Studies -- 3.3.1. Parametric Analysis -- 3.3.2. Stall Speed-Cruise Speed Carpet Plot -- 3.3.3. Design of Experiments -- 3.4. Introduction to Design Optimization -- 3.4.1. Fundamental Concepts -- 3.4.2. More on Objective Functions -- 3.4.3. Linear Programming -- 3.4.4. Nonlinear Surfaces and Lagrange Multipliers -- 3.4.5. Wing Sizing Optimization by Example -- Exercises -- References -- Chapter 4: Aircraft Configuration Layout -- 4.1. Introduction -- 4.1.1. The Content of This Chapter -- 4.1.2. Requirements, Mission, and Applicable Regulations -- 4.1.3. How to Design a Good Aircraft -- 4.1.4. Summary of Common Configuration Targets -- 4.1.5. Past and Present Directions in Aircraft Design -- 4.1.6. Aircraft Component Recognition -- 4.2. The Fundamentals of the Configuration Layout -- 4.2.1. Vertical Wing Location -- 4.2.2. Wing Configuration -- 4.2.3. Wing Dihedral -- 4.2.4. Wing Structural Configuration -- 4.2.5. Cabin Configuration -- 4.2.6. Propeller Configuration -- 4.2.7. Engine Placement.. - 4.2.8. Landing Gear Configuration -- 4.2.9. Tail Configuration -- 4.2.10. Configuration Decision Matrix -- References -- Chapter 5: Aircraft Structural Layout -- 5.1. Introduction -- 5.1.1. The Content of This Chapter -- 5.1.2. Notes on Aircraft Loads -- 5.2. Aircraft Fabrication and Materials -- 5.2.1. The Basics of Material Properties -- 5.2.2. Various Fabrication Methods -- 5.2.3. Aluminum Alloys -- 5.2.4. Steel Alloys -- 5.2.5. Titanium Alloys -- 5.2.6. Composite Materials -- 5.3. Airframe Structural Layout -- 5.3.1. Important Structural Concepts -- 5.3.2. Fundamental Layout of the Wing Structure -- 5.3.3. Fundamental Layout of the Horizontal and Vertical Tail Structures -- 5.3.4. Fundamental Layout of the Fuselage Structure -- References -- Chapter 6: Aircraft Weight Analysis -- 6.1. Introduction -- 6.1.1. The Content of This Chapter -- 6.1.2. Definitions -- 6.1.3. Fundamental Weight Relations -- 6.2. Initial Weight Analysis Methods -- 6.2.1. Method 1: Initial Gross Weight Estimation Using Historical Relations -- 6.2.2. Method 2: Historical Empty Weight Fractions -- 6.2.3. Method 3: Initial Gross Weight Estimation Using Mission Analysis -- 6.3. Secondary Weight Analysis Methods -- 6.4. Statistical Weight Estimation Methods -- 6.4.1. Weight of Aircraft Components-GA Aircraft -- 6.4.2. Estimating Engine Weight -- 6.5. Direct Weight Estimation Methods -- 6.5.1. Direct Weight Estimation for a Wing -- 6.5.2. Variation of Weight with AR -- 6.6. Inertia Properties -- 6.6.1. Fundamentals -- 6.6.2. Reference Locations -- 6.6.3. Total Weight -- 6.6.4. Moment About (x0, y0, y0) -- 6.6.5. Center-of-Mass, Center-of-Gravity, Centroid of a Volume -- 6.6.6. Determination of CG Location by Aircraft Weighing -- 6.6.7. Mass Moment of Inertia -- 6.6.8. Mass Product of Inertia -- 6.6.9. Principal Moments of Inertia -- 6.6.10. Inertia Matrix.. - 6.7. The Center-of-Gravity Envelope -- 6.7.1. Fundamentals -- 6.7.2. Creating the CG-Envelope -- 6.7.3. Loading Cloud -- 6.7.4. In-Flight Movement of the CG -- 6.7.5. Weight Budgeting -- 6.7.6. Weight Tolerancing -- Exercises -- References -- Chapter 7: Selecting the Powerplant -- 7.1. Introduction -- 7.1.1. The Content of This Chapter -- 7.1.2. Factors Affecting the Selection of the Powerplant -- 7.1.3. The Basics of Energy, Work, and Power -- 7.1.4. Fundamental Definitions -- 7.1.5. Fuel Basics -- 7.1.6. On the Thermodynamics of the Powerplant -- 7.2. Piston Engines -- 7.2.1. Fundamental Definitions -- 7.2.2. Basic Theory of Internal Combustion Engines -- 7.2.3. The Use of Gearboxes -- 7.2.4. Extracting Piston Power From Engine Performance Charts -- 7.2.5. Extracting Piston Power Using the Petty Equation -- 7.2.6. Piston Engine Installation -- 7.2.7. Piston Engine Inlet and Exit Sizing -- 7.3. Gas Turbine Engines -- 7.3.1. Topics Specific to Turboprops -- 7.3.2. Topics Specific to Turbojets -- 7.3.3. Topics Specific to Turbofans -- 7.3.4. Installation of Gas Turbines -- 7.3.5. Subsonic Inlet Design -- 7.4. Electric Motors and Battery Technology -- 7.4.1. Basic Formulas of Electricity -- 7.4.2. Battery Basics -- 7.4.3. Additional Sources of Electric Energy -- 7.4.4. Electric Motor Basics -- Exercises -- References -- Chapter 8: The Anatomy of the Airfoil -- 8.1. Introduction -- 8.1.1. The Content of This Chapter -- 8.1.2. Dimensional Analysis-Buckinghams Pi-Theorem -- 8.1.3. Representation of Forces and Moments -- 8.1.4. Properties of Typical Airfoils -- 8.1.5. The Pressure Coefficient -- 8.1.6. Chordwise Pressure Distribution -- 8.1.7. Forces and Moment per Unit Span -- 8.1.8. Center of Pressure and Aerodynamic Center -- 8.1.9. The Generation of Lift -- 8.1.10. Boundary Layer Basics -- 8.1.11. Airfoil Stall Characteristics.. - 8.1.12. Analysis of Ice Accretion on Airfoils -- 8.1.13. Designations of Common Airfoils -- 8.1.14. Airfoil Design -- 8.2. The Geometry of the Airfoil -- 8.2.1. Airfoil Terminology -- 8.2.2. NACA 4-Digit Airfoils -- 8.2.3. NACA 5-Digit Airfoils -- 8.2.4. NACA 1-Series Airfoils -- 8.2.5. NACA 6-Series Airfoils -- 8.2.6. NACA 7-Series Airfoils -- 8.2.7. NACA 8-Series Airfoils -- 8.2.8. Plotting NACA 4- and 5-Digit Airfoils -- 8.2.9. Summary of NACA Airfoils -- 8.2.10. Selected Famous Airfoils -- 8.3. The Force and Moment Characteristics of the Airfoil -- 8.3.1. The Effect of Camber -- 8.3.2. The Effect of Reynolds Number -- 8.3.3. The Effect of Early Flow Separation -- 8.3.4. The Effect of a Trailing-Edge Flap -- 8.3.5. The Effect of a Slot or Slats -- 8.3.6. The Effect of Deploying a Spoiler -- 8.3.7. The Effect of Leading-Edge Roughness and Surface Smoothness -- 8.3.8. The Effect of Compressibility -- 8.3.9. Decision Matrix for Airfoil Selection -- Exercises -- References -- Chapter 9: The Anatomy of the Wing -- 9.1. Introduction -- 9.1.1. The Content of This Chapter -- 9.1.2. Definition of Reference Area -- 9.1.3. The Process of Wing Sizing -- 9.2. The Trapezoidal Wing Planform -- 9.2.1. Geometric Formulation of an Arbitrary Planform -- 9.2.2. Geometric Formulation of the Trapezoidal Planform -- 9.2.3. Geometric Formulation of a Cranked Planform -- 9.2.4. Poor Mans Determination of the MGC -- 9.2.5. Planform Dimensions in Terms of S, AR, and λ -- 9.2.6. Wing Volume Approximation -- 9.3. The Geometric Layout of the Wing -- 9.3.1. Wing Aspect Ratio -- 9.3.2. Wing Taper Ratio, TR or λ -- 9.3.3. Wing Sweep Angle, Λ -- 9.3.4. Dihedral and Anhedral, Γ -- 9.3.5. Wing Twist-Washout and Washin, phi -- 9.3.6. Wing Angle-of-Incidence, iW -- 9.3.7. Wing Layout Properties of Selected Aircraft -- 9.4. Planform Selection.. - 9.4.1. Methods to Present Spanwise Lift Distribution.
Emner
Sjanger
Dewey
ISBN
0-12-822647-1

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