| タイトル | Aeroacoustic Characteristics of Model Jet Test Facility Flow Conditioners |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050182104 |
| 著者（英） | Henderson, Brenda S.; Kinzie, Kevin W.; Haskin, Harry H. |
| 著者所属（英） | NASA Langley Research Center |
| 発行日 | 2005-01-01 |
| 言語 | eng |
| 内容記述 | An experimental investigation of flow conditioning devices used to suppress internal rig noise in high speed, high temperature experimental jet facilities is discussed. The aerodynamic and acoustic characteristics of a number of devices including pressure loss and extraneous noise generation are measured. Both aerodynamic and acoustic characteristics are strongly dependent on the porosity of the flow conditioner and the closure ratio of the duct system. For unchoked flow conditioners, the pressure loss follows conventional incompressible flow models. However, for choked flow conditioners, a compressible flow model where the duct and flow conditioner system is modeled as a convergent-divergent nozzle can be used to estimate pressure loss. Choked flow conditioners generate significantly more noise than unchoked conditioners. In addition, flow conditioners with small hole diameters or sintered metal felt material generate less self-noise noise compared to flow conditioners with larger holes. |
| NASA分類 | Acoustics |
| レポートNO | AIAA Paper 2005-3055 |
| 権利 | No Copyright |
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