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METHOD AND DEVICE FOR DETERMINING CRITICAL BUFFETING LOADS ON A STRUCTURE OF AN AIRCRAFT

  • US 20100312497A1
  • Filed: 05/27/2010
  • Published: 12/09/2010
  • Est. Priority Date: 06/03/2009
  • Status: Active Grant
First Claim
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1. A method for determining critical loads generated by buffeting on a structure (S) of an airplane (A), said method comprising:

  • a) conducting trials in a blowing unit on an airplane model, said trials comprising;

    simulating conditions for which some flow burble occurs on at least one part of a surface of the airplane (A); and

    carrying out, for such conditions, measurements using stationary pressure sensors, instationary pressure sensors and accelerometers arranged on said model;

    b) using at least some of such measurements, the flow burble areas are determined on said structure (S) of the airplane (A);

    c) implementing an aerodynamic model for determining, using the measurements from steps a), in the flow burble areas as determined from step b), a pressure field resulting in the structure (S) buffeting;

    d) integrating the determined pressure field so as to obtain the overall stresses and moments generated by buffeting;

    e) calculating, using such overall stresses and moments, the stresses that the structure (S) is to bear, such stresses comprising aerodynamic stresses caused by buffeting, induced aerodynamic stresses, inertia stresses and damping stresses; and

    f) determining the critical loads due to buffeting using the stresses as calculated in step e).

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