| タイトル | Critical Low-Noise Technologies Being Developed for Engine Noise Reduction Systems Subproject |
| 本文（外部サイト） | http://hdl.handle.net/2060/20050192148 |
| 著者（英） | Grady, Joseph E.; Civinskas, Kestutis C. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2004-05-01 |
| 言語 | eng |
| 内容記述 | NASA's previous Advanced Subsonic Technology (AST) Noise Reduction Program delivered the initial technologies for meeting a 10-year goal of a 10-dB reduction in total aircraft system noise. Technology Readiness Levels achieved for the engine-noise-reduction technologies ranged from 4 (rig scale) to 6 (engine demonstration). The current Quiet Aircraft Technology (QAT) project is building on those AST accomplishments to achieve the additional noise reduction needed to meet the Aerospace Technology Enterprise's 10-year goal, again validated through a combination of laboratory rig and engine demonstration tests. In order to meet the Aerospace Technology Enterprise goal for future aircraft of a 50- reduction in the perceived noise level, reductions of 4 dB are needed in both fan and jet noise. The primary objectives of the Engine Noise Reduction Systems (ENRS) subproject are, therefore, to develop technologies to reduce both fan and jet noise by 4 dB, to demonstrate these technologies in engine tests, and to develop and experimentally validate Computational Aero Acoustics (CAA) computer codes that will improve our ability to predict engine noise. |
| NASA分類 | Aircraft Propulsion and Power |
| 権利 | No Copyright |
|
