Aircraft Conceptual Design Synthesis means design by fitness-for-purpose. Design engineers can jump off from the point of given parameters and requirements – required performance, payloads and other factors.
This is the first book for the aeronautical designer devoted to guiding the reader through this highly effective conceptual design synthesis process. This forms the procedure for the initial stage of the aircraft design process – the interpretation of a requirement into the preliminary layout. A logical design sequence is developed utilizing original modules to represent propulsion, lift, drag, mass, and performance. Aircraft Conceptual Design Synthesis includes a disk of spreadsheets that provides core data. Unlike existing approaches, the design synthesis method can be applied to novel aircraft concepts.
CONTENTS INCLUDE
“This is an important landmark book and in my view will become a standard by which others will be compared” – Dr E C P Ransom, Kingston University, UK
Aircraft Conceptual Design Synthesis
Conceptual Design Synthesis and Optimization for New Generations of Combat Aircraft
The author of this book, Mr. E. Torenbeek, has made a large contribution to this part of the study programme for many years.
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.
This project consists of designing and implementing a real-time graphical interface for a workstation-based flight simulator.
Davenport, T.H. and Prusak, L., “Working Knowledge – How Organisations Manage What They Know,” Harvard Business School Press, 1998. Miles, J. and Moore, C., “Practical Knowledge-Based Systems in Conceptual Design,” First Edition, ...
Introduction to Aeronautics: A Design Perspective
S. Culley. Aircraft Conceptual Design Synthesis By Denis Howe This is the first book for the aeronautical designer devoted to guiding the reader through this highly effective conceptual design synthesis process . Aircraft Conceptual Design ...
Cruise fuel: Fuel = W0 – W1 = Wf(eR/k – 1), where k, the range constant, equals L/D (V/SFC). ... A6.2 shows a simplified method to predict cruise drag for civil jet transports, which was extracted from Loftin [60].
8 Abzug, M.J. and Larrabee, E.E. (2002). Aircraft Stability and Control. Cambridge, UK: Cambridge Aerospace Press. ... IHS ESDU, 133 Houndsditch, London 13 Talay, T. A (1976). NASA SP-367; Introduction to the Aerodynamics of Flight.