Noise generation by shock-turbulence interaction
October 1970
| Main Authors: | , , |
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| Other Authors: | |
| Format: | Technical Report |
| Published: |
Cambridge, Mass. : Gas Turbine Laboratory , Massachusetts Institute of Technology, [1970]
2016
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| Online Access: | http://hdl.handle.net/1721.1/104691 |
| _version_ | 1826193524808220672 |
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| author | Kiang, David Tien Sik Tam, Christopher Kwong Wah Kerrebrock, Jack L. |
| author2 | Massachusetts Institute of Technology. Gas Turbine Laboratory |
| author_facet | Massachusetts Institute of Technology. Gas Turbine Laboratory Kiang, David Tien Sik Tam, Christopher Kwong Wah Kerrebrock, Jack L. |
| author_sort | Kiang, David Tien Sik |
| collection | MIT |
| description | October 1970 |
| first_indexed | 2024-09-23T09:40:30Z |
| format | Technical Report |
| id | mit-1721.1/104691 |
| institution | Massachusetts Institute of Technology |
| last_indexed | 2024-09-23T09:40:30Z |
| publishDate | 2016 |
| publisher | Cambridge, Mass. : Gas Turbine Laboratory , Massachusetts Institute of Technology, [1970] |
| record_format | dspace |
| spelling | mit-1721.1/1046912019-04-11T09:01:17Z Noise generation by shock-turbulence interaction Kiang, David Tien Sik Tam, Christopher Kwong Wah Kerrebrock, Jack L. Massachusetts Institute of Technology. Gas Turbine Laboratory Jet planes -- Noise Shock waves Turbulence October 1970 Includes bibliographical references (leaf 10) The noise produced by convection of turbulence through an oblique shock wave has been measured and compared to theoretical predictions by Ribner and Kerrebrock. There is excellent agreement with the theoretical prediction that, for a fixed turbulent input, the downstream noise pressure (divided by the mean pressure), should first increase very rapidly, and then decrease as the normal Mach number of the shock is increased from unity to values of the order of 1.5. This behavior implies that a part of the noise from supersonic jets should behave similarly, with a sharp increase, then a decrease as the nozzle pressure ratio is raised from unity. This Research Carried Out in the Gas Turbine Laboratory, M.I.T., in Cooperation with Lewis Research Center, NASA, under Grant NGL 22-009-383 2016-10-06T21:22:00Z 2016-10-06T21:22:00Z 1970 Technical Report http://hdl.handle.net/1721.1/104691 09673913 GTL report #102 10 leaves application/pdf Cambridge, Mass. : Gas Turbine Laboratory , Massachusetts Institute of Technology, [1970] |
| spellingShingle | Jet planes -- Noise Shock waves Turbulence Kiang, David Tien Sik Tam, Christopher Kwong Wah Kerrebrock, Jack L. Noise generation by shock-turbulence interaction |
| title | Noise generation by shock-turbulence interaction |
| title_full | Noise generation by shock-turbulence interaction |
| title_fullStr | Noise generation by shock-turbulence interaction |
| title_full_unstemmed | Noise generation by shock-turbulence interaction |
| title_short | Noise generation by shock-turbulence interaction |
| title_sort | noise generation by shock turbulence interaction |
| topic | Jet planes -- Noise Shock waves Turbulence |
| url | http://hdl.handle.net/1721.1/104691 |
| work_keys_str_mv | AT kiangdavidtiensik noisegenerationbyshockturbulenceinteraction AT tamchristopherkwongwah noisegenerationbyshockturbulenceinteraction AT kerrebrockjackl noisegenerationbyshockturbulenceinteraction |