Lysak et al., 2013 - Google Patents
Prediction of high frequency gust response with airfoil thickness effectsLysak 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 …
- 230000000694 effects 0 title description 28
Classifications
-
- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
- G06F17/00—Digital computing or data processing equipment or methods, specially adapted for specific functions
- G06F17/50—Computer-aided design
- G06F17/5009—Computer-aided design using simulation
- G06F17/5018—Computer-aided design using simulation using finite difference methods or finite element methods
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