| タイトル | Studies of the acoustic transmission characteristics of coaxial nozzles with inverted velocity profiles: Comprehensive data report |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790019762 |
| 著者（英） | Salikuddin, M.; Mungur, P.; Dean, P. D.; Ahuja, K. K.; Plumblee, H. E. |
| 著者所属（英） | Lockheed-Georgia Co. |
| 発行日 | 1979-05-01 |
| 言語 | eng |
| 内容記述 | The efficiency of internal noise radiation through a coannular exhaust nozzle with an inverted velocity profile was studied. A preliminary investigation was first undertaken (1) to define the test parameters which influence the internal noise radiation; (2) to develop a test methodology which could realistically be used to examine the effects of the test parameters; and (3) to validate this methodology. The result was the choice of an acoustic impulse as the internal noise source in the jet nozzles. Noise transmission characteristics of a coannular nozzle system were then investigated. In particular, the effects of fan convergence angle, core extension length to annulus height ratio and flow Mach numbers and temperatures were studied. Relevant spectral data only is presented in the form of normalized nozzle transfer function versus nondimensional frequency. |
| NASA分類 | ACOUSTICS |
| レポートNO | 79N27933
NASA-CR-159628 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/175028 |
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