NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Core-Noise ResearchThis presentation is a technical summary of and outlook for NASA-internal and NASA-sponsored external research on core noise funded by the Fundamental Aeronautics Program Subsonic Fixed Wing (SFW) Project. Sections of the presentation cover: the SFW system-level noise metrics for the 2015 (N+1), 2020 (N+2), and 2025 (N+3) timeframes; SFW strategic thrusts and technical challenges; SFW advanced subsystems that are broadly applicable to N+3 vehicle concepts, with an indication where further noise research is needed; the components of core noise (compressor, combustor and turbine noise) and a rationale for NASAʼs current emphasis on the combustor-noise component; the increase in the relative importance of core noise due to turbofan design trends; the need to understand and mitigate core-noise sources for high-efficiency small gas generators; and the current research activities in the core-noise area, with additional details given about forthcoming updates to NASAʼs Aircraft Noise Prediction Program (ANOPP) core-noise prediction capabilities, two NRA efforts (Honeywell International, Phoenix, AZ and University of Illinois at Urbana-Champaign, respectively) to improve the understanding of core-noise sources and noise propagation through the engine core, and an effort to develop oxide/oxide ceramic-matrix-composite (CMC) liners for broadband noise attenuation suitable for turbofan-core application. Core noise must be addressed to ensure that the N+3 noise goals are met. Focused, but long-term, core-noise research is carried out to enable the advanced high-efficiency small gas-generator subsystem, common to several N+3 conceptual designs, needed to meet NASAʼs technical challenges. Intermediate updates to prediction tools are implemented as the understanding of the source structure and engine-internal propagation effects is improved. The NASA Fundamental Aeronautics Program has the principal objective of overcoming today's national challenges in air transportation. The SFW Quiet-Aircraft Subproject aims to develop concepts and technologies to reduce perceived community noise attributable to aircraft with minimal impact on weight and performance. This reduction of aircraft noise is critical to enabling the anticipated large increase in future air traffic.
Document ID
20150010125
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Hultgren, Lennart S.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
June 8, 2015
Publication Date
March 13, 2012
Subject Category
Aircraft Design, Testing And Performance
Acoustics
Meeting Information
Meeting: NASA Fundamental Aeronautics 2012 Technical Conference
Location: Cleveland, OH
Country: United States
Start Date: March 13, 2012
End Date: March 15, 2012
Sponsors: NASA Glenn Research Center
Funding Number(s)
WBS: WBS 561581.02.08.03.45.02.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available