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Beschreibung
Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This volume details the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane.
It covers trajectory analysis, stability, and control. In addition, the volume presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Throughout, a subsonic business jet is used as an example for the calculations presented in the book.
It covers trajectory analysis, stability, and control. In addition, the volume presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Throughout, a subsonic business jet is used as an example for the calculations presented in the book.
Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This volume details the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane.
It covers trajectory analysis, stability, and control. In addition, the volume presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Throughout, a subsonic business jet is used as an example for the calculations presented in the book.
It covers trajectory analysis, stability, and control. In addition, the volume presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Throughout, a subsonic business jet is used as an example for the calculations presented in the book.
Zusammenfassung
Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This text is concerned with the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane. It presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Once an analytical solution has been obtained, numbers are calculated in order to compare the answer with the assumptions used to derive it and to acquaint readers with the sizes of the numbers. A subsonic business jet is used for these calculations.
Inhaltsverzeichnis
to Airplane Flight Mechanics.- 3DOF Equations of Motion.- Atmosphere, Aerodynamics, and Propulsion.- Cruise and Climb of an Arbitrary Airplane.- Cruise and Climb of an Ideal Subsonic Airplane.- Take-off and Landing.- PS and Turns.- 6DOF Model: Wind Axes.- Static Stability and Control.- 6DOF Model: Body Axes.- Dynamic Stability and Control.
Details
Erscheinungsjahr: | 2010 |
---|---|
Fachbereich: | Raumfahrttechnik |
Genre: | Technik |
Rubrik: | Naturwissenschaften & Technik |
Medium: | Taschenbuch |
Seiten: | 312 |
Inhalt: |
xiii
298 S. 125 s/w Illustr. 25 s/w Tab. |
ISBN-13: | 9783642079870 |
ISBN-10: | 3642079873 |
Sprache: | Englisch |
Ausstattung / Beilage: | Paperback |
Einband: | Kartoniert / Broschiert |
Autor: | Hull, David G. |
Auflage: | Softcover reprint of hardcover 1st ed. 2007 |
Hersteller: |
Springer-Verlag GmbH
Springer Berlin Heidelberg |
Maße: | 235 x 155 x 17 mm |
Von/Mit: | David G. Hull |
Erscheinungsdatum: | 14.10.2010 |
Gewicht: | 0,476 kg |
Zusammenfassung
Flight mechanics is the application of Newton's laws to the study of vehicle trajectories (performance), stability, and aerodynamic control. This text is concerned with the derivation of analytical solutions of airplane flight mechanics problems associated with flight in a vertical plane. It presents algorithms for calculating lift, drag, pitching moment, and stability derivatives. Once an analytical solution has been obtained, numbers are calculated in order to compare the answer with the assumptions used to derive it and to acquaint readers with the sizes of the numbers. A subsonic business jet is used for these calculations.
Inhaltsverzeichnis
to Airplane Flight Mechanics.- 3DOF Equations of Motion.- Atmosphere, Aerodynamics, and Propulsion.- Cruise and Climb of an Arbitrary Airplane.- Cruise and Climb of an Ideal Subsonic Airplane.- Take-off and Landing.- PS and Turns.- 6DOF Model: Wind Axes.- Static Stability and Control.- 6DOF Model: Body Axes.- Dynamic Stability and Control.
Details
Erscheinungsjahr: | 2010 |
---|---|
Fachbereich: | Raumfahrttechnik |
Genre: | Technik |
Rubrik: | Naturwissenschaften & Technik |
Medium: | Taschenbuch |
Seiten: | 312 |
Inhalt: |
xiii
298 S. 125 s/w Illustr. 25 s/w Tab. |
ISBN-13: | 9783642079870 |
ISBN-10: | 3642079873 |
Sprache: | Englisch |
Ausstattung / Beilage: | Paperback |
Einband: | Kartoniert / Broschiert |
Autor: | Hull, David G. |
Auflage: | Softcover reprint of hardcover 1st ed. 2007 |
Hersteller: |
Springer-Verlag GmbH
Springer Berlin Heidelberg |
Maße: | 235 x 155 x 17 mm |
Von/Mit: | David G. Hull |
Erscheinungsdatum: | 14.10.2010 |
Gewicht: | 0,476 kg |
Warnhinweis