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北京石油化工学院2026年研究生招生接收调剂公告
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[资源] 【转贴】Aircraft Design【以搜无重复】

斯坦福大学讲课内容整理而成

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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 AuthorsIlan 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 the Advanced Research Projects Agency on high altitude long endurance aircraft. 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 president of Desktop Aeronautics, Inc. and is an advanced-rated hang glider pilot.
Richard Shevell was the original author of several of these chapters. 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.

This version of Aircraft Design: Synthesis and Analysis is intended for use with Netscape Navigator, version 4.0 or later, or with Microsoft's Internet Explorer, version 4.0 or later. The text makes use of frames, , and Java, so be sure your browser supports this and that these features are enabled. Please see the help available from Netscape or Microsoft for using the browser software.
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We have minimized the use of embedded hypertext links as we have found this often confuses students trying to navigate through a textbook. It also makes it difficult to expand or delete sections to form a custom version of the text (see below). This means that most of the navigation is done through the table of contents. A rather complete table of contents can also be found in the prefatory information and active links on this page will also work. Some hypertext links are used, but most are restricted to single level pages with additional detail, as might be found in an extended footnote.

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