McHugh et al., 2021 - Google Patents
Flutter and limit cycle oscillations of cantilevered plate in supersonic flowMcHugh et al., 2021
View PDF- Document ID
- 7480507328177752199
- Author
- McHugh K
- Freydin M
- Bastos K
- Beran P
- Dowell E
- Publication year
- Publication venue
- Journal of Aircraft
External Links
Snippet
Research interest is growing for theoretical models of highly deflected structures in aeroelastic settings. Presented here is a model of a cantilevered plate subjected to axial supersonic flow to determine the flutter boundary and postflutter characteristics of a system …
- 230000004048 modification 0 abstract description 11
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- 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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- G—PHYSICS
- G06—COMPUTING; CALCULATING; COUNTING
- G06F—ELECTRICAL DIGITAL DATA PROCESSING
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- G06F17/504—Formal methods
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- G06—COMPUTING; CALCULATING; COUNTING
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- G06F17/50—Computer-aided design
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- G06F17/5036—Computer-aided design using simulation for analog modelling, e.g. for circuits, spice programme, direct methods, relaxation methods
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- G06F17/13—Differential equations
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- 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
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- G06F17/5086—Mechanical design, e.g. parametric or variational design
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- G06F2217/16—Numerical modeling
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- G06F—ELECTRICAL DIGITAL DATA PROCESSING
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- G06F2217/80—Thermal analysis and optimization
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