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Quiet, Efficient Fans for Spaceflight: An Overview of NASA's Technology Development PlanA Technology Development Plan to improve the aerodynamic and acoustic performance of spaceflight fans has been submitted to NASA s Exploration Technology Development Program. The plan describes a research program intended to make broader use of the technology developed at NASA Glenn to increase the efficiency and reduce the noise of aircraft engine fans. The goal is to develop a set of well-characterized government-owned fans nominally suited for spacecraft ventilation and cooling systems. NASA s Exploration Life Support community will identify design point conditions for the fans in this study. Computational Fluid Dynamics codes will be used in the design and analysis process. The fans will be built and used in a series of tests. Data from aerodynamic and acoustic performance tests will be used to validate performance predictions. These performance maps will also be entered into a database to help spaceflight fan system developers make informed design choices. Velocity measurements downstream of fan rotor blades and stator vanes will also be collected and used for code validation. Details of the fan design, analysis, and testing will be publicly reported. With access to fan geometry and test data, the small fan industry can independently evaluate design and analysis methods and work towards improvement.
Document ID
20100023320
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Koch, L. Danielle
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
May 1, 2010
Subject Category
Acoustics
Report/Patent Number
NC10-075
NASA/TM-2010-216238
E-17225
Report Number: NC10-075
Report Number: NASA/TM-2010-216238
Report Number: E-17225
Meeting Information
Meeting: NOISE-CON 2010
Location: Baltimore, MD
Country: United States
Start Date: April 19, 2010
End Date: April 21, 2010
Sponsors: Institute of Noise Control Engineering
Funding Number(s)
WBS: WBS 439906.04.01.02.02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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