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Marti et al., 2017 - Google Patents

Multiple equilibrium points of airfoil flutter in viscous flow

Marti et al., 2017

Document ID
3850501799781009868
Author
Marti F
Liu F
Publication year
Publication venue
55th AIAA Aerospace Sciences Meeting

External Links

Snippet

The Isogai NACA 64A010 airfoil model 1 is a classic 2D flutter problem. Although being a 2D case, the structural properties are defined such that the airfoil represents a section of a swept wing with a pitching point ahead of the leading edge. This problem has been …
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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
    • G—PHYSICS
    • G06—COMPUTING; CALCULATING; COUNTING
    • G06F—ELECTRICAL DIGITAL DATA PROCESSING
    • G06F2217/00—Indexing scheme relating to computer aided design [CAD]
    • G06F2217/16—Numerical modeling

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