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Lysak et al., 2013 - Google Patents

Prediction of high frequency gust response with airfoil thickness effects

Lysak et al., 2013

Document ID
11942638812309611703
Author
Lysak P
Capone D
Jonson M
Publication year
Publication venue
Journal of Fluids and Structures

External Links

Snippet

The unsteady lift forces that act on an airfoil in turbulent flow are an undesirable source of vibration and noise in many industrial applications. Methods to predict these forces have traditionally treated the airfoil as a flat plate. At higher frequencies, where the relevant …
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Classifications

    • GPHYSICS
    • G06COMPUTING; CALCULATING; COUNTING
    • G06FELECTRICAL DIGITAL DATA PROCESSING
    • G06F17/00Digital computing or data processing equipment or methods, specially adapted for specific functions
    • G06F17/50Computer-aided design
    • G06F17/5009Computer-aided design using simulation
    • G06F17/5018Computer-aided design using simulation using finite difference methods or finite element methods

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