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If fan aerodynamic and acoustic performance is important to your project, don’t hesitate to contact us. We’ll be happy to discuss your concerns, our capabilities, and explore possibilities for collaborative research. Please contact:

E. Brian Fite
216-433-3892

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Collaboration
FOCUS ON FANS
Quiet, efficient fan systems are the result of painstaking attention to detail. Put a quiet fan into a poorly designed system, and fan aerodynamic and acoustic performance will suffer. Likewise, there are few easy system changes that can be made to compensate for an intrinsically noisy fan. Identifying dominant mechanisms for noise generation in a fan system and prescribing effective noise reduction methods are not simple tasks. Understanding the fundamental physics of fan aeroacoustics, and translating what we’ve learned into practical diagnostic, design, and analysis tools has been a primary focus of the NASA Glenn Acoustics Branch.

NASA Glenn has facilities, instrumentation, and experimental hardware to test a range of fans. The 9’ x15’ Low Speed Wind Tunnel has been used extensively to study the aerodynamic and acoustic performance of aircraft engine fan stages. The Advanced Noise Control Fan Rig has been used to develop active noise control systems. And the anechoic environments of the Acoustical Testing Laboratory and the Aero-Acoustic Propulsion Laboratory can be used to support specialized testing for smaller fans destined for use in spaceflight systems.

Researchers at NASA Glenn continue to develop both Fan Tone Noise Prediction Software and Fan Broadband Noise Prediction Software. These tools can be used in a variety of ways. Some schemes employ a number of simplifying assumptions, run quickly, and are suitable for trend studies and conceptual design work. Modeling fan problems more realistically often requires more detailed input (usually from an Euler or Navier-Stokes solver) and is more computationally intensive. Only validated software is useful, which is why we compare our predictions against data. Specialized instrumentation like rotating microphone rakes, hot wire probes, Laser Doppler Velocimetry, and Particle Image Velocimetry helps us get measurements we need.

Researchers at NASA Glenn are well connected and often collaborate with engineers in industry, universities, and other NASA Centers:
NASA Johnson Acoustics Office
NASA Ames Experimental Physics Branch
NASA Langley Aeroacoustics Branch
NASA Langley Structural Acoustics Branch
Involving industrial and academic partners in basic research accelerates tech transfer and inspires the next generation.

Related Papers

+ An Assessment of NASA Glenn's Aeroacoustic Experimental and Predictive Capabilities for Installed Cooling Fans, Part 1: Aerodynamic Performance
Dale E. Van Zante, L. Danielle Koch, Mark P. Wernet, Gary G. Podboy
+ Slides from the presentation at InterNoise 2006

+ An Assessment of NASA Glenn's Aeroacoustic Experimental and Predictive Capabilities for Installed Cooling Fans, Part 2: Source Identification and Validation
L. Danielle Koch, Dale E. Van Zante, Mark P. Wernet, Gary G. Podboy
+ Slides from the presentation at InterNoise 2006

+ Cool and Quiet: Partnering to Enhance the Aerodynamic and Acoustic Performance of Installed Electronics Cooling Fans: A White Paper
L. Danielle Koch, Dale E. Van Zante

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+ On-site Far Field Noise     Measurments
SMALL FAN RESOURCES
Developing quiet, efficient fan systems for spaceflight or for cooling electronics here on Earth is challenging. Check out our resource list for small fan aerodynamics and acoustics.

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NASA Official: E. Brian Fite
Last Updated: July 8, 2008


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