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Case Studies for the Statistical Design of Experiments Applied to Powered Rotor Wind Tunnel Tests
2015
31st AIAA Aerodynamic Measurement Technology and Ground Testing Conference
unpublished
The application of statistical Design of Experiments (DOE) to helicopter wind tunnel testing was explored during two powered rotor wind tunnel entries during the summers of 2012 and 2013. These tests were performed jointly by the U.S. Army Aviation Development Directorate Joint Research Program Office and NASA Rotary Wing Project Office, currently the Revolutionary Vertical Lift Project, at NASA Langley Research Center located in Hampton, Virginia. Both entries were conducted in the 14-by
doi:10.2514/6.2015-2713
fatcat:7zca6f7ah5ctjp7tu7vaetnkwa