Halila et al., 2016 - Google Patents
Numerical study on transitional flows using a correlation-based transition modelHalila et al., 2016
View PDF- Document ID
- 12119818197514806724
- Author
- Halila G
- Bigarella E
- Azevedo J
- Publication year
- Publication venue
- Journal of Aircraft
External Links
Snippet
A correlation-based transition model is assessed against distinct test cases. The configurations include a zero-pressure-gradient flat plate, a single-element aeronautical airfoil, a multielement high-lift airfoil and a wing–body configuration. These test cases are …
- 230000000694 effects 0 abstract description 30
Classifications
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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
- 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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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/02—Wind tunnels
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