The new edition of this popular textbook provides a modern, accessible introduction to the whole process of aircraft design from requirements to conceptual design, manufacture and in-service issues. Highly illustrated descriptions of the full spectrum of aircraft types, their aerodynamics, structures and systems, allow students to appreciate good and poor design and understand how to improve their own designs. Cost data is considerably updated, many new images have been added and new sections are included on the emerging fields of Uninhabited Aerial Vehicles and environmentally-friendly airlines. Examples from real aircraft projects are presented throughout, demonstrating to students the applications of the theory. Three appendices and a bibliography provide a wealth of information, much not published elsewhere, including simple aerodynamic formulae, an introduction to airworthiness and environmental requirements, aircraft, engine and equipment data, and a case study of the conceptual design of a large airliner.
This new edition provides a modern, accessible introduction to the whole process of aircraft design together with invaluable data.
Introduction to Aircraft Design South Asia Edition
Find the right answer the first time with this useful handbook of preliminary aircraft design.
The author of this book, Mr. E. Torenbeek, has made a large contribution to this part of the study programme for many years.
This book presents the entire process of aircraft design based on a systems engineering approach from conceptual design phase, through to preliminary design phase and to detail design phase.
Introduction to Aeronautics: A Design Perspective
Advanced Aircraft Design: Conceptual Design, Analysis and Optimization of Subsonic Civil Airplanes presents a quasi-analytical optimization approach based on a concise set of sizing equations.
A self-contained in-depth treatment of aircraft performance, designed for a first course in aeronautical or aerospace engineering for undergraduate engineers. Provides an understanding of why conventional aircraft look and fly...
Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics.
16 Uanishi, K., Pearson, N. S, Lahnig, T. R. and Leon, R. M. (1991). CFD based 3-D turbofan nacelle design system. AIAA Paper No: A91–16278. 17 Laban, M. (2003). Application of CFD to drag analysis and validation with wind tunnel Data.