Title: Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, and Classical Feedback Control (AIAA Education Series)
Publisher: Amer Inst of Aeronautics &
Publication Date: 2003
Language: English
ISBN 10: 1563475774
ISBN 13: 9781563475771
Binding: Hardcover
Condition: As New
Weight: 37 ounces

About this title

Synopsis

This new textbook is based on a successful 15-year approach to teaching aircraft flight mechanics at the U.S. Air Force Academy.

Intended for junior-level students presented with the material for the first time, the book clearly explains all the concepts and derivations of equations for aircraft flight mechanics. The material progresses through aircraft performance, static stability, aircraft dynamic stability, and feedback control. The chapters present real world applications and contain problems.

Each year the Academy's students are placed with industry, NASA, and Air Force labs and test organizations during the summer immediately following their junior year. The hosts are asked to provide feedback on how well the students are prepared in the fields of flight mechanics and aerodynamics. Each year, the student reviews are outstanding, illustrating the excellent quality of the authors' approach.

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