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Advisors: Hilario Montes, Javier

Department-Institute: Universidad Carlos III de Madrid. Departamento de Bioingeniería e Ingeniería Aeroespacial

Degree: Ingeniería Aeroespacial

Issued date: 2015-09

Defense date: 2015-10-16

Keywords: Aircrafts , Structural load analysis

Rights: Atribución-NoComercial-SinDerivadas 3.0 España

Abstract:Structural load analysis relates the calculation and determination of the loadsthat act in the aircraft for its manoeuvres, landing, turbulence flight

.This project has the aim to study and synthesize the parameters and manoeuvresthat size the horizontaStructural load analysis relates the calculation and determination of the loadsthat act in the aircraft for its manoeuvres, landing, turbulence flight

.This project has the aim to study and synthesize the parameters and manoeuvresthat size the horizontal tailplane for a preliminary design. This is performedwith a combination of structural equations as well as analytical calculation reachinga graphical representation of the dependency of the parameters for different situationsin the flighting envelope of the aircraft.The analysis performed and discussed might be understood as a general methodthat may need the inclusion of significant parameters for a particular configurationthat have been neglected in the equations of the analysis in order to simplified theformulations.+-





Autor: Girón Carrero, Marta

Fuente: http://e-archivo.uc3m.es



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