Publication: Parametric sizing of HTP flight loads
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Publication date
2015-09
Defense date
2015-10-16
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Abstract
Structural 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.
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Keywords
Aircrafts, Structural load analysis