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NACA-TM-3123
Effect of various arrangements of triangular ledges on the performance of a 23 degree conical diffuser at subsonic Mach numbers
Year: 1954
Abstract: A brief investigation has been made to determine whether the use of annular ledges to promote turbulent momentum exchange will improve the performance of a short, wide-angle diffuser. Results are presented of tests of a 23º conical diffuser with a 2:1 ratio of exit to inlet area with both rough and smooth triangular ledges, approximately one-tenth of the inlet boundary-layer thickness in height, installed in succession from the inlet to the exit. The results show that, although the flow in the diffuser without ledges was very unstable, the presence of a roughness strip near the inlet, with or without additional ledges, assured stable flow. For the configurations investigated, the static-pressure recovery and the total-pressure-loss coefficient were either unaffected or only slightly impaired by the installation of the ledges.
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| contributor author | NASA - National Aeronautics and Space Administration (NASA) | |
| date accessioned | 2017-09-04T16:57:56Z | |
| date available | 2017-09-04T16:57:56Z | |
| date copyright | 01/01/1954 | |
| date issued | 1954 | |
| identifier other | BWONEEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/121335 | |
| description abstract | A brief investigation has been made to determine whether the use of annular ledges to promote turbulent momentum exchange will improve the performance of a short, wide-angle diffuser. Results are presented of tests of a 23º conical diffuser with a 2:1 ratio of exit to inlet area with both rough and smooth triangular ledges, approximately one-tenth of the inlet boundary-layer thickness in height, installed in succession from the inlet to the exit. The results show that, although the flow in the diffuser without ledges was very unstable, the presence of a roughness strip near the inlet, with or without additional ledges, assured stable flow. For the configurations investigated, the static-pressure recovery and the total-pressure-loss coefficient were either unaffected or only slightly impaired by the installation of the ledges. | |
| language | English | |
| title | NACA-TM-3123 | num |
| title | Effect of various arrangements of triangular ledges on the performance of a 23 degree conical diffuser at subsonic Mach numbers | en |
| type | standard | |
| page | 37 | |
| status | Active | |
| tree | NASA - National Aeronautics and Space Administration (NASA):;1954 | |
| contenttype | fulltext |