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Aircraft Design: Synthesis and Analysis ~ Version 0.99
#1
This material is based on course notes for the class AA241A and B, a
graduate level course in aircraft design at Stanford University. The
course involves individual aircraft design projects with problem sets
and lectures devoted to various aspects of the design and analysis of a
complete aerospace system. Students select a particular type of aircraft
to be designed and, in two academic quarters, define the configuration
using methods similar to those used in the aircraft industry for
preliminary design work. Together with the vehicle definition and
analysis, basic principles of applied aerodynamics, structures,
controls, and system integration, applicable to many types of aerospace
problems are discussed. The objective of the course is to present the
fundamental elements of these topics, showing how they are applied in a
practical design.




About the Authors

[تصویر:  kroo.gif]
Ilan Kroo is a Professor of Aeronautics and Astronautics at Stanford
University. He received a degree in Physics from Stanford in 1978, then
continued graduate studies in Aeronautics, leading to a Ph.D. degree in
1983. He worked in the Advanced Aerodynamic Concepts Branch at NASA's
Ames Research Center then returned to Stanford as a member of the
Aero/Astro faculty. Prof. Kroo's research in aerodynamics and aircraft
design has focussed on the study of innovative airplane concepts and
multidisciplinary optimization. He has participated in the design of
high altitude aircraft, human-powered airplanes, America's Cup
sailboats, and high-speed research aircraft. He was one of the principal
designers of the SWIFT, tailless sailplane design and has worked with
government teams on several UAV programs. He directs a research group at
Stanford consisting of about ten Ph.D. students and teaches aircraft
design and applied aerodynamics at the graduate level. In addition to
his research and teaching interests, Prof. Kroo is Chief Scientist of
Desktop Aeronautics, Inc. and the Aerion Corporation, and is an
advanced-rated hang glider pilot.


Richard Shevell was the original author of many parts of these
notes. He worked in aerodynamics and design at Douglas Aircraft Company
for 30 years, was head of advanced design during the development of the
DC-9 and DC-10, and taught at Stanford University after that for 20
years. To a large extent, this is his course






Rar'd PDF ~ 570 Pages,bookmarked

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http://rapidshare.com/files/14672607...aft_Design.rar
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