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
مبلغ قابل پرداخت 30,000 تومان
برچسب های مهم