科技报告详细信息
| Simulations of the Nasa Langley 14- by 22-Foot Subsonic Tunnel for the Juncture Flow Experiment | |
| Lee, Henry ; Pulliam, Thomas ; Rumsey, Chris ; Carlson, Jan-Renee | |
| 关键词: BOUNDARY LAYER THICKNESS; COMPUTATIONAL FLUID DYNAMICS; COMPUTERIZED SIMULATION; FLUID DYNAMICS; HORSESHOE VORTICES; SUBSONIC WIND TUNNELS; TURBULENCE MODELS; WIND EFFECTS; WIND TUNNEL TESTS; | |
| RP-ID : ARC-E-DAA-TN55088 | |
| 美国|英语 | |
| 来源: NASA Technical Reports Server | |
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| Files | Size | Format | View |
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| 20190025480.pdf | 4414KB |  download |
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