Browsing Gas Turbine Laboratory by Subject "Aeroelasticity -- Mathematical models"

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    • Optimal mistuning for enhanced aeroelastic stability of transonic fans 

      Hall, Kenneth C.; Crawley, Edward F. ([Washington, D.C.? : National Aeronautics and Space Administration, 1983], 1983)
      An inverse design procedure was developed for the design of a mistuned rotor. The design requirements are that the stability margin of the eigenvalues of the aeroelastic system be greater than or equal to some minimum ...