Feb. 25, 2008

AE 332 Aircraft Design  3 0 0 6

Introduction to Aircraft Design: Three phases in aircraft design, computer based aircraft design methodologies, differences between LTA and HTA aircraft, type of civil and military aircraft.

Configuration and Layout: Types and comparison of wing, tail, fuselage,
landing gear, wing-tail combinations, powerplant (types, numbers,
locations), unconventional aircraft configurations.

Sizing and Constraint Analysis: Initial sizing, estimation of design gross weight, rubber engine sizing
and fixed engine sizing, refined sizing method and constraint analysis.

Estimation Methodologies: Lift and drag coefficient, design loads,
component mass breakdown, acquisition cost, direct operating cost.

Operational and Environmental Issues: Range-payload diagram, V-n diagram,
noise and emission levels, special considerations such as stealth,
survivability, maintainability.

Advanced Concepts in Aircraft Design: supersonic aircraft design, very large aircraft, morphing aircraft.


Books:
1) D. P. Raymer, Aircraft Design - A Conceptual Approach, AIAA
Educational Series, 4th Ed., 2006.

2) S. A. Brandt, R. J. Stiles, J. J. Bertin, R. Whitford, Introduction to Aeronautics: A Design Perspective, AIAA Educational Series, 2nd ed., 2004.

3) L. R., Jenkinson, P. Simpkin & D. Rhodes, Civil Jet Aircraft Design, Arnold Publishers, London, 1999.

4) J. Fielding, Introduction to Aircraft Design, Cambridge Aerospace
Series, Cambridge University Press, 1999.