Navigabilité des aéronefs

Aircraft Architecture and Load Calculation

Objectives

To provide the methods and means of calculating load distribution in the various parts of an aircraft (wings, fuselage, landing gear, etc.) as a function of its multiple operating phases, in order to determine the sizing of the structures.

Educational content

Architecture and calculation of structures

Wings and control surfaces.

Fuselage.

Assemblies.

Design philosophy.

Calculation of loads

In-flight loads

Flight envelope.

Symmetrical manoeuvres.

Dissymmetrical manoeuvres.

Gusts.

Ground loads

Landing.

Ground manoeuvres.

Fatigue of aeronautical structures

Damage tolerance.

Note :

A visit to the structures activity of C.E.A.T. may also be organised.

For information only  : 27 hours

Participates

Engineers and executives.
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