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Open Rotor DevelopmentThe ERA project executed a comprehensive test program for Open Rotor aerodynamic and acoustic performance. System studies used the data to estimate the fuel burn savings and acoustic margin for an aircraft system with open rotor propulsion. The acoustic measurements were used to produce an auralization that compares the legacy blades to the current generation of open rotor designs.
Document ID
20160014870
Acquisition Source
Glenn Research Center
Document Type
Presentation
Authors
Van Zante, Dale E. (NASA Glenn Research Center Cleveland, OH United States)
Rizzi, Stephen A. (NASA Langley Research Center Hampton, VA United States)
Date Acquired
December 29, 2016
Publication Date
March 29, 2016
Subject Category
Aeronautics (General)
Report/Patent Number
GRC-E-DAA-TN30402
Report Number: GRC-E-DAA-TN30402
Meeting Information
Meeting: Green Aviation Technical Interchange Meeting (TIM)
Location: Hampton, VA
Country: United States
Start Date: March 29, 2016
Sponsors: NASA Headquarters
Funding Number(s)
WBS: WBS 338881.02.07.03.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Open Rotors
Acoustics
Propellers

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