Introduction to Aircraft Flight Mechanics.

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.

Bibliographic Details
Call Number:Libro Electrónico
Main Author: Yechout, Thomas R.
Other Authors: Staff, American Institute of Aeronautics and Astronautics
Format: Electronic eBook
Language:Inglés
Published: Reston : American Institute of Aeronautics and Astronautics, 2000.
Series:AIAA education series.
Subjects:
Airplanes > Performance.
Aerodynamics.
Flight.
Flight control.
Avions > Performances.
Aérodynamique.
Vol.
Systèmes de commande (Vol)
aerodynamics.
Aerodynamics
Airplanes > Performance
Flight
Flight control
Flugmechanik
Flugleistung
Flugstabilität
Online Access:Texto completo
Description
Summary: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.
Physical Description:1 online resource (650 pages)
Bibliography:Includes bibliographical references (page 623) and index.
ISBN:9781600860782
1600860788

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