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Introduction to Aircraft Flight Mechanics
Thomas R. Yechout
其他書名
Performance, Static Stability, Dynamic Stability, and Classical Feedback Control
出版AIAA, 2003
ISBN16008607889781600860782
URLhttp://books.google.com.hk/books?id=a_c2V0zAFwcC&hl=&source=gbs_api
EBookSAMPLE
註釋Based on a 15-year successful approach to teaching aircraft flight mechanics at the US Air Force Academy, this text explains the concepts and derivations of equations for aircraft flight mechanics. It covers aircraft performance, static stability, aircraft dynamics stability and feedback control.