Articoli correlati a Introduction to Aircraft Flight Mechanics: Performance,...

Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, Classical Feedback Control, and State-space Foundations - Rilegato

Libro 101 di 124: AIAA Education

Yechout, Thomas R.

 
9781624102547: Introduction to Aircraft Flight Mechanics: Performance, Static Stability, Dynamic Stability, Classical Feedback Control, and State-space Foundations
Rilegato
ISBN 10: 1624102549 ISBN 13: 9781624102547
Casa editrice: Amer Inst of Aeronautics &, 2014

Sinossi

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.

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Editore
Amer Inst of Aeronautics &
Data di pubblicazione
2014
Lingua
Inglese
ISBN 10 
1624102549
ISBN 13 
9781624102547
Rilegatura
Copertina rigida
Numero edizione
2
Numero di pagine
700
Contatto del produttore
non disponibile
Persona responsabile
non disponibile