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FUNDAMENTAL NOISE NASA GLENN RESEARCH CENTER Loretta Shaw, Subsonic Systems Office

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Propulsion Systems Program. FUNDAMENTAL NOISE NASA GLENN RESEARCH CENTER Loretta Shaw, Subsonic Systems Office Dennis Huff, Acoustic Branch Chief. Propulsion Systems Program. Aerospace Propulsion and Power Base Program. Propulsion Fundamentals Research Project. - PowerPoint PPT Presentation
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FUNDAMENTAL NOISE NASA GLENN RESEARCH CENTER Loretta Shaw, Subsonic Systems Office Dennis Huff, Acoustic Branch Chief Propulsion Systems Program
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Page 1: FUNDAMENTAL NOISE NASA GLENN RESEARCH CENTER Loretta Shaw, Subsonic Systems Office

FUNDAMENTAL NOISE

NASA GLENN RESEARCH CENTER

Loretta Shaw, Subsonic Systems OfficeDennis Huff, Acoustic Branch Chief

Propulsion Systems Program

Page 2: FUNDAMENTAL NOISE NASA GLENN RESEARCH CENTER Loretta Shaw, Subsonic Systems Office

Aerospace Propulsion and Power Base Program

Objective: Develop advanced concepts to reduce subsonic engine fan, jet and core noise.

Fundamental Noise

Propulsion Fundamentals Research Project

Objective: …to provide support for new high-risk, high-payoffactivities that are of long term strategic importance

Propulsion Systems Program

Aeroacoustic Propulsion Laboratory

Page 3: FUNDAMENTAL NOISE NASA GLENN RESEARCH CENTER Loretta Shaw, Subsonic Systems Office

• Jet Noise Experiments - Provide fundamental insight into physics of jet noise generation and propagation

Aerospace Propulsion and Power Base Program

Propulsion Systems Program

Fundamental Noise Approach in FY00

Small Hot Acoustic Jet Rig

• Fan Noise Prediction- Develop the next generation fan noise prediction tools

based on Computational Aeroacoustics

• Jet Noise Prediction- Develop next generation jet noise prediction tools based on modeling and Computational Aeroacoustics

MGBKprediction

Data

Page 4: FUNDAMENTAL NOISE NASA GLENN RESEARCH CENTER Loretta Shaw, Subsonic Systems Office

ï Micro-blown Acoustic Aft-duct Splitter - Demonstrate the reduction of skin friction and aft duct fan noise with a micro-blown aft duct splitter

Aerospace Propulsion and Power Base Program

Propulsion Systems Program

Fundamental Noise Approach in FY00 Continued

ï Advanced Fan Noise Reduction Concept- Design a 2-staged low tip speed fan with swept stator vanes and

synchrophased fans to obtain active noise cancellation

ï Active Control of Fan Broadband Noise- Develop a technique to actively control fan broadband noise

Source cross-correlation studies


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