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.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Yechout, Thomas R.
Otros Autores: Staff, American Institute of Aeronautics and Astronautics
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Reston : American Institute of Aeronautics and Astronautics, 2000.
Colección:AIAA education series.
Temas:
Airplanes > Performance.
Aerodynamics.
Flight.
Flight control.
Avions > Performances.
Aérodynamique.
Vol.
Systèmes de commande (Vol)
aerodynamics.
Aerodynamics
Airplanes > Performance
Flight
Flight control
Flugmechanik
Flugleistung
Flugstabilität
Acceso en línea:Texto completo
Descripción
Sumario: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.
Descripción Física:1 online resource (650 pages)
Bibliografía:Includes bibliographical references (page 623) and index.
ISBN:9781600860782
1600860788

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