Year: 2017
Type: article
Abstract: During February 2017, aerodynamic and acoustic testing was performed on a scale-model high bypass ratio turbofan rotor, R4, in an internal flow component test facility. An overview of the testing completed is presented.
Authors: Rick Bozak, Gary Podboy, Robert P. Dougherty
Institutions: Glenn Research Center, Optinav (United States)
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: green
OpenAlex ID: W2733097464