UID:
almahu_9949698077202882
Format:
1 online resource (1146 pages)
Edition:
Second edition.
ISBN:
0-12-822647-1
Content:
"General Aviation Aircraft Design, Second Edition, continues to be the engineer’s best source for answers to realistic aircraft design questions. The book has been expanded to provide design guidance for additional classes of aircraft, including seaplanes, biplanes, UAS, high-speed business jets, and electric airplanes. In addition to conventional powerplants, design guidance for battery systems, electric motors, and complete electric powertrains is offered."--
Note:
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.
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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.
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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.
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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.
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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.
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9.4.1. Methods to Present Spanwise Lift Distribution.
Additional Edition:
ISBN 0-12-818465-5
Language:
English
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