Core/Combustor-Noise Baseline Measurements for the DGEN Aeropropulsion Research Turbofan
Author:
Affiliation:
1. NASA Glenn Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2018-3281
Reference6 articles.
1. An Analytical Assessment of NASA's N+1 Subsonic Fixed Wing Project Noise Goal
2. 3Hultgren, L. S. “A First Look at the DGEN380 Engine Acoustic Data From a Core-Noise Perspective,” Tech. Rep. NASA/TM-2015-218924, NASA, 2015.
3. Designing Clean Jet-Noise Facilities and Making Accurate Jet-Noise Measurements
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