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Article | REF: TRP4032 V1

Structural loads in flight - Aircraft flight area

Author: Yves GOURINAT

Publication date: May 10, 2015

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2. Load-bearing surfaces

2.1 External aerodynamic loads

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2.1.1 Aerodynamic resultant

First, we define the aircraft axes (structure axes or fuselage axes) as follows (figure 4 ):

  • x→ unit vector along the longitudinal axis, directed forward ;

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