Fundamentals of Aircraft and Airship Design (AIAA Education Series)

CONTENTS
Preface
Chapter 1 - Introduction
Chapter 2 - Review of Practical Aerodynamics
Chapter 3 - Aircraft Performance Methods
Chapter 4 - Aircraft Operating Envelope
Chapter 5 - Preliminary Estimate of Takeoff Weight
Chapter 6 - Estimating the Takeoff Wing Loading
Chapter 7 - Selecting the Planform and Airfoil Section
Chapter 8 - Preliminary Fuselage Sizing and Design
Chapter 9 - High-Life Devices
Chapter 10 - Takeoff and Landing Analysis
Chapter 11 - Preliminary Sizing of the Vertical and Horizontal Tails
Chapter 12 - Designing for Survivability (Stealth)
Chapter 13 - Estimating Wing-Body Aerodynamics
Chapter 14 - Propulsion System Fundamentals
Chapter 15 - Turbine Engine Inlet Design
Chapter 16 - Corrections for Turbine Engine Installation
Chapter 17 - Propeller Propulsion Systems
Chapter 18 - Propulsion System Thrust Sizing
Chapter 19 - Structures and Materials
Chapter 20 - Refined Weight Estimate
Chapter 21 - Static Stability and Control
Chapter 22 - Trim Drag and Maneuvering Flight
Chapter 23 - Control Surface Sizing Criteria
Chapter 24 - Life Cycle Cost
Chapter 25 - Trade Studies and Sizing
Appendix A - Conversions
Appendix B - Atmospheric Data
Appendix C - Isentropic Compressible Flow Functions
Appendix D - Normal Shock Functions for a Perfect Gas
Appendix E - Plane Oblique and Conical Shocks
Appendix F - NACA Airfoil Nomenclature and Data
Appendix G - Aerodynamic Data of Real Aircraft
Appendix H - Aerodynamics of Wing Body Combinations
Appendix I - Aircraft Weights Data
Appendix J - Propulsion Data
Appendix K - Miscellaneous Data