AIRCRAFT DESIGN: A CONCEPTUAL APPROACH 3RD EDITION

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Ouvrage 1-56347-281-3 : AIRCRAFT DESIGN: A CONCEPTUAL APPROACH 3RD EDITION
Author's Note
Design---A Separate Discipline What Is Design?
Introduction to the Book Overview of the Design Process Introduction
Phases of Aircraft Design Aircraft Conceptual Design Process Integrated Product Development and Aircraft Design
Sizing from a Conceptual sketch Introduction
Takeoff-Weight Buildup Empty-Weight Estimation Fuel-Fraction Estimation Takeoff-Weight Calculation Design Example: Asw Aircraft Airfoil and Geometry Selection Introduction
Airfoil Selection
Wing Geometry
Biplane Wings
Tail Geometry and Arrangement Thrust-to-Weight Ratio and Wing Loading Introduction
Thrust-to-Weight Ratio Wing Loading
Selection of Thrust-to-Weight and Wing Loading
Initial Sizing
Introduction
Rubber-Engine Sizing Fixed-Engine Sizing Geometry Sizing
Control-Surface Sizing Configuration Layout and Loft Introduction
End Products of Configuration Layout Conic Lofting
Conic Fuselage Development Flat-Wrap Fuselage Lofting Circle-to-Square Adapter Fuselage Loft Verification Wing/Tail Layout and Loft Wetted Area Determination Volume Determination Use of CAD in Conceptual Design Special Considerations in Configuration Layout Introduction
Aerodynamic Considerations Structural Considerations Radar Detectability Infrared Detectability Visual Detectability Aural Signature
Vulnerability Considerations Crashworthiness Considerations Producibility Considerations Maintainability Considerations Crew Station, Passengers, and Payload Introduction
Crew Station
Passenger compartment Cargo Provisions
Weapons Carriage
Gun Installation
Propulsion and Fuel System Integration Introduction
Propulsion Selection Jet-Engine Integration Propeller-Engine Integration Fuel System
Landing Gear and Subsystems Introduction
Landing Gear Arrangements Tire Sizing
Shock Absorbers
Castoring-Wheel Geometry Gear-Retraction Geometry Seaplanes
Subsystems
INTERMISSION: STEP-BY-STEP DEVELOPMENT OF A NEW DESIGN Aerodynamics
Introduction
Aerodynamic Forces Aerodynamic Coefficients Lift
Parasite (Zero-Lift) Drag Drag Due to Lift (Induced Drag) Aerodynamic Codes and Computational Fluid Dynamics (CFD) Propulsion Introduction
Jet-Engine Thrust Considerations Turbojet Installed Thrust Thrust-Drag Bookkeeping Installed-Thrust Methodology Piston-Engine Performance Turboprop Performance Structures and Loads Introduction
Loads Categories
Air Loads
Inertial Loads
Powerplant Loads
Landing-Gear Loads Structures Fundamentals Material Selection Material Properties Structural-Analysis Fundamentals Finite-Element Structural Analysis Weights Introduction
Approximate Group Weights Method Statistical Group Weights Method Additional Considerations in Weights Estimation Stability, Control, and Handling Qualities Introduction
Coordinate Systems and Definitions Longitudinal Static Stability and Control Lateral-Directional Static Stability and Control
Stick-Free Stability Effects of Flexibility Dynamic Stability
Quasi-Steady State Inertia Coupling
Handling Qualities Performance and Flight Mechanics Introduction and Equations of Motion Steady Level Flight Steady Climbing and Descending Flight Level Turning Flight Gliding Flight
Energy-Maneuverability Methods Operating Envelope Takeoff Analysis
Landing Analysis
Other Fighter Performance Measures of Merit Cost Analysis
Introduction
Elements of Life-Cycle Cost Cost-Estimating Methods RDT&E and Production Costs Operations and Maintenance Costs Cost Measures of Merit (Military) Aircraft and Airline Economics Sizing and Trade Studies Introduction
Detailed Sizing Methods Improved Conceptual Sizing Methods Sizing Matrix and Carpet Plots Trade Studies
Design of Unique Aircraft Concepts Introduction
Jet VTOL
Prop VTOL and Helicopter Hypersonic Vehicles Flying Wing, Tailless, Lifting Fuselage, and Blended Wing-Body Delta and Double-Delta Wing Forward-Swept Wing Canard-Pusher
Multi-Fuselage
Asymmetrical
Joined Wing
Wing-in-Ground Effect Unmanned/Uninhabited Conceptual Design Examples Introduction
Single-Seat Aerobatic Lightweight Supercruise Fighter Appendix A. Unit Conversion Appendix B. Standard Atmosphere, Compressible Flow, and Shocks B.1 Standard Atmosphere B.2 Compressible Flow Tables B.3 Shock Charts
Appendix C. Airspeed C.1 Airspeed Relationships C.2 Airspeed Conversion Charts Appendix D. Airfoil Data Appendix E. Typical Engine Performance Curves E.1 Afterburning Turbofan E.2 High-Bypass Turbofan E.3 Turboprop
Appendix F. Design Requirements and Specifications References
Questions
Index


Auteur : RAYMER
Editeur : AMERICAN INSTITUTE
Nombre de pages : 923
Date de publication : 06 1999

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