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http://worldcat.org/entity/work/id/19369111

Application of a supersonic kernel-function procedure to flutter analysis of thin lifting surfaces

A description is presented of a systematic procedure for obtaining generalized aerodynamic forces from the lifting-surface theory by the supersonic kernel-function method and for using those forces thus obtained in a Galerkin modal flutter analysis. The method is applicable to planforms with subsonic leading and supersonic trailing edges. Analytical flutter results were obtained and compared with experimental values from three flutter models.

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  • "A description is presented of a systematic procedure for obtaining generalized aerodynamic forces from the lifting-surface theory by the supersonic kernel-function method and for using those forces thus obtained in a Galerkin modal flutter analysis. The method is applicable to planforms with subsonic leading and supersonic trailing edges. Analytical flutter results were obtained and compared with experimental values from three flutter models."@en

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  • "Application of a supersonic kernel-function procedure to flutter analysis of thin lifting surfaces"@en
  • "Application of a supersonic kernel-function procedure to flutter analysis of thin lifting surfaces"

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