Introduction to Aircraft Flight Mechanics

Introduction to Aircraft Flight Mechanics Performance, Static Stability, Dynamic Stability, Classical Feedback Control, and State-Space Foundations - AIAA Education Series

Second edition

Hardback (30 Jun 2014)

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Publisher's Synopsis

Introduction to Aircraft Flight Mechanics, Second Edition revises and expands this acclaimed, widely adopted textbook. Outstanding for use in undergraduate aeronautical engineering curricula, it is written for those first encountering the topic by clearly explaining the concepts and derivations of equations involved in aircraft flight mechanics. The text begins with a review of basic aerodynamics and propulsion and continues through aircraft performance, equations of motion, static stability, linearizing equations of motion, dynamic stability, classical feedback control, stability and control augmentation, Bode, state space, and special topics. The second edition also features insights about the A-10 based upon the author's career experience with this aircraft. Past winner of the AIAA Summerfield Book Award, this text contributes greatly to learning the fundamental principles of flight mechanics that are a crucial foundation of any aeronautical engineering curricula. It contains both real world applications and problems. A solutions manual is available to instructors by contacting AIAA.

Book information

ISBN: 9781624102547
Publisher: American Institute of Aeronautics & Astronautics
Imprint: AIAA
Pub date:
Edition: Second edition
DEWEY: 629.132
DEWEY edition: 23
Language: English
Number of pages: xvii, 700
Weight: 1306g
Height: 239mm
Width: 163mm
Spine width: 39mm