Hilario Montes, JavierGirón Carrero, Marta2016-09-192016-09-192015-092015-10-16https://hdl.handle.net/10016/23593Structural load analysis relates the calculation and determination of the loads that act in the aircraft for its manoeuvres, landing, turbulence flight... This project has the aim to study and synthesize the parameters and manoeuvres that size the horizontal tailplane for a preliminary design. This is performed with a combination of structural equations as well as analytical calculation reaching a graphical representation of the dependency of the parameters for different situations in the flighting envelope of the aircraft. The analysis performed and discussed might be understood as a general method that may need the inclusion of significant parameters for a particular configuration that have been neglected in the equations of the analysis in order to simplified the formulations.application/pdfengAtribución-NoComercial-SinDerivadas 3.0 EspañaAircraftsStructural load analysisbachelor thesisAeronáuticaopen access