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The birth of airplane stability theory

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The birth of airplane stability theory

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dc.contributor.author Magraner Rullan, José Pedro es_ES
dc.contributor.author Martinez-Val, R. es_ES
dc.date.accessioned 2016-04-20T11:44:29Z
dc.date.available 2016-04-20T11:44:29Z
dc.date.issued 2014-07
dc.identifier.issn 0954-4100
dc.identifier.uri http://hdl.handle.net/10251/62773
dc.description.abstract Airplane stability theory was born at the end of the XIX century and matured around 100 years ago, when airplanes were hardly controllable yet. The success and safety of flights in the pioneer years depended upon largely unknown stability and control characteristics. Understanding the modes of airplane motion has been of paramount importance for the development of aviation. The contributions made by a few scientists in the decades preceding and following the first flight by the Wright brothers set the concepts and equations that, with minor notation aspects, have remained almost unchanged till present day. es_ES
dc.language Inglés es_ES
dc.publisher SAGE Publications (UK and US) es_ES
dc.relation.ispartof Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering es_ES
dc.rights Reserva de todos los derechos es_ES
dc.subject Aviation history es_ES
dc.subject Airplane stability es_ES
dc.subject Phugoid es_ES
dc.subject Pioneer flight dynamics es_ES
dc.subject.classification INGENIERIA AEROESPACIAL es_ES
dc.title The birth of airplane stability theory es_ES
dc.type Artículo es_ES
dc.identifier.doi 10.1177/0954410013494139
dc.rights.accessRights Abierto es_ES
dc.contributor.affiliation Universitat Politècnica de València. Departamento de Máquinas y Motores Térmicos - Departament de Màquines i Motors Tèrmics es_ES
dc.description.bibliographicCitation Magraner Rullan, JP.; Martinez-Val, R. (2014). The birth of airplane stability theory. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 228(9):1498-1506. doi:10.1177/0954410013494139 es_ES
dc.description.accrualMethod S es_ES
dc.relation.publisherversion http://dx.doi.org/10.1177/0954410013494139 es_ES
dc.description.upvformatpinicio 1498 es_ES
dc.description.upvformatpfin 1506 es_ES
dc.type.version info:eu-repo/semantics/publishedVersion es_ES
dc.description.volume 228 es_ES
dc.description.issue 9 es_ES
dc.relation.senia 288472 es_ES
dc.description.references PERKINS, C. D. (1970). Development of airplane stability and control technology /1970 Von Karman Lecture/. Journal of Aircraft, 7(4), 290-301. doi:10.2514/3.44167 es_ES
dc.description.references Abzug, M. J., & Larrabee, E. E. (2002). Airplane Stability and Control, Second Edition. doi:10.1017/cbo9780511607141 es_ES
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dc.description.references Wegener, P. P. (1997). What Makes Airplanes Fly? doi:10.1007/978-1-4612-2254-5 es_ES
dc.description.references Pradeep, S., & Kamesh, S. (1999). Does the Phugoid Frequency Depend on Speed? Journal of Guidance, Control, and Dynamics, 22(2), 372-373. doi:10.2514/2.4391 es_ES
dc.description.references Phillips, W. F. (2000). Phugoid Approximation for Conventional Airplanes. Journal of Aircraft, 37(1), 30-36. doi:10.2514/2.2586 es_ES
dc.description.references Pamadi, B. N. (2004). Performance, Stability, Dynamics, and Control of Airplanes, Second Edition. doi:10.2514/4.862274 es_ES
dc.description.references Ananthkrishnan, N., & Ramadevi, P. (2002). Consistent Approximations to Aircraft Longitudinal Modes. Journal of Guidance, Control, and Dynamics, 25(4), 820-824. doi:10.2514/2.4952 es_ES
dc.description.references McRuer, D. T., Graham, D., & Ashkenas, I. (1990). Aircraft Dynamics and Automatic Control. doi:10.1515/9781400855988 es_ES


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