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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:
Acceso en línea:Texto completo

MARC

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100 1 |a Yechout, Thomas R. 
245 1 0 |a Introduction to Aircraft Flight Mechanics. 
260 |a Reston :  |b American Institute of Aeronautics and Astronautics,  |c 2000. 
300 |a 1 online resource (650 pages) 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a AIAA education series 
588 0 |a Print version record. 
505 0 |a ""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Acknowledgments""; ""Chapter 1. A Review of Basic Aerodynamics""; ""Chapter 2. A Review of Basic Propulsion""; ""Chapter 3. Aircraft Performance""; ""Chapter 4. Aircraft Equations of Motion""; ""Chapter 5. Aircraft Static Stability""; ""Chapter 6. Linearizing the Equations of Motion""; ""Chapter 7. Aircraft Dynamic Stability""; ""Chapter 8. Classical Feedback Control""; ""Chapter 9. Aircraft Stability and Control Augmentation""; ""Appendix A. Conversions"" 
505 8 |a ""Appendix B. Properties of the U.S. Standard Atmosphere""""Appendix C. Airfoil Data""; ""Appendix D. T-38 Performance Data""; ""Appendix E. Selected Laplace Transforms""; ""Appendix F. Cramerâ€?s Rule""; ""Appendix G. Development of Longitudinal and Lateralâ€?Directional Transfer Functions""; ""Appendix H. Stability Characteristics of Selected Aircraft""; ""Bibliography""; ""Index""; ""Series listing"" 
504 |a Includes bibliographical references (page 623) and index. 
520 |a 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. 
590 |a ProQuest Ebook Central  |b Ebook Central Academic Complete 
650 0 |a Airplanes  |x Performance. 
650 0 |a Aerodynamics. 
650 0 |a Flight. 
650 0 |a Flight control. 
650 6 |a Avions  |x Performances. 
650 6 |a Aérodynamique. 
650 6 |a Vol. 
650 6 |a Systèmes de commande (Vol) 
650 7 |a aerodynamics.  |2 aat 
650 7 |a Aerodynamics  |2 fast 
650 7 |a Airplanes  |x Performance  |2 fast 
650 7 |a Flight  |2 fast 
650 7 |a Flight control  |2 fast 
650 7 |a Flugmechanik  |2 gnd 
650 7 |a Flugleistung  |2 gnd 
650 7 |a Flugstabilität  |2 gnd 
700 1 |a Staff, American Institute of Aeronautics and Astronautics. 
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776 0 8 |i Print version:  |a Yechout, Thomas R.  |t Introduction to Aircraft Flight Mechanics.  |d Reston : American Institute of Aeronautics and Astronautics, ©2000  |z 9781563475771 
830 0 |a AIAA education series. 
856 4 0 |u https://ebookcentral.uam.elogim.com/lib/uam-ebooks/detail.action?docID=3111652  |z Texto completo 
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994 |a 92  |b IZTAP