کتابخانه

کتابخانه

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Fundamentals of Aircraft and Airship Design, Volume I - Aircraft Design


Fundamentals of Aircraft and Airship Design, Volume I - Aircraft Design

Title: Fundamentals of Aircraft and Airship Design, Volume I - Aircraft Design | Author(s): Nicolai, Leland M.; Carichner, Grant E. | Publisher: American Institute of Aeronautics and Astronautics | Year: 2010 | Language: English | Pages : 945 | ISBN: 978-1-61344-046-9, 978-1-60086-751-4 | Size: 34 MB | Extension: pdf

 

The aircraft is only a transport mechanism for the payload, and all design decisions must consider payload first. Simply stated, the aircraft is a dust cover. This book emphasizes that the aircraft design process is a science and an art, but also a compromise. The authors address the conceptual design phase comprehensively, for both civil and military aircraft, from initial consideration of user needs, material selection, and structural arrangement to the decision to iterate the design one more time. The book includes designing for survivability (stealth), solar- and human-powered aircraft systems, and very high altitude operation with air breathing propulsion. This book revises and expands the 1975 classic aircraft design textbook that has been used worldwide for more than 30 years. Completely updated with the latest industry processes and techniques, it will benefit graduate and upper-level undergraduate students as well as practicing engineers. Special features include step-by-step examples throughout the book, including designing a wing, lessons captured from historical case studies of aircraft design, and full-color photographs of multiple aircraft. - Data and information appearing in this book are for informational purposes only. AIAA and the author are not responsible for any injury or damage resulting from use or reliance, nor do AIAA and the author warrant that use or reliance will be free from privately owned rights.

 

Table of 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-Lift 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

  • Index

  • Supporting Materials


 


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