Du et al., 2022 - Google Patents
Investigation on the three-dimensional shock wave/turbulence boundary layer control induced by the secondary recirculation jetsDu et al., 2022
View PDF- Document ID
- 48249697874531379
- Author
- Du Z
- Shen C
- Huang W
- Shen Y
- Wu H
- Han Y
- Publication year
- Publication venue
- Computers & Fluids
External Links
Snippet
The interaction between the shock wave and the turbulence boundary layer induces a separation, and this is an undesired phenomenon for the flow field performance. The control work of the separation is pretty important. In the current study, the passive control is carried …
- 230000035939 shock 0 title abstract description 89
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
- 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
- G06F17/504—Formal methods
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