Aero-Thermal Performance of a Winglet at Engine Representative Mach and Reynolds Numbers
Year: 2010
Type: conference-paper
DOI: 10.1115/gt2010-22794
Institutions: University of Oxford, Rolls-Royce (United Kingdom)
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: closed
OpenAlex ID: W2122992009
