NASA NTRS · 20160014870
Open Rotor Development
Abstract
The 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.
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Van Zante, Dale E., Rizzi, Stephen A.. 2016-03-29. Open Rotor Development. https://ntrs.nasa.gov/citations/20160014870
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