Item type | Current library | Home library | Collection | Shelving location | Call number | Status | Barcode | |
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American University in Dubai | American University in Dubai | Non-fiction | Main Collection | TL 671.2 .S3136 2013 (Browse shelf(Opens below)) | Available | 5153166 |
TL 570 .K76 1998 Foundations of aerodynamics : bases of aerodynamic design / | TL 570 .P46 2010 Mechanics of flight / | TL 670.3 .B38 2000 100 historic airplanes in full color / | TL 671.2 .S3136 2013 Aircraft design : a systems engineering approach / | TL 674 .G68 2003 Fundamentals of structural integrity : damage tolerant design and nondestructive evaluation / | TL 681.C3 V56 2011 Aircraft Interior Comfort and Design / | TL 695 .F85 2014 Airborne electronic hardware design assurance : a practitioner's guide to RTCA/DO-254 / |
Includes bibliographical references and index.
1. Aircraft design fundamentals -- 2. Systems engineering approach -- 3. Aircraft conceptual design -- 4. Preliminary design -- 5. Wing design -- 6. Tail design -- 7. Fuselage design -- 8. Propulsion system design -- 9. Landing gear design -- 10. Weight of components -- 11. Aircraft weight distribution -- 12. Design of control surfaces -- Appendices.
"Presenting in one volume the methodologies behind aircraft design, this book uses a systems engineering approach to cover the components and the issues affected by design procedures. The basic topics that are essential to the process, such as aerodynamics and controls, are covered first of all. The author then explains the design process in a holistic manner to emphasize the integration of individual components into the overall design. Throughout the book, the various design options are considered and weighed against each other, to give readers a practical understanding of the process overall"--
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