Noise Radiation from a Continuous Mold-Line Link Flap Configuration
نویسندگان
چکیده
منابع مشابه
Wind Tunnel Investigation of a Flexible Wing High-Lift Configuration with a Variable Camber Continuous Trailing Edge Flap Design
Nhan T. Nguyen a NASA Ames Research Center, Moffett Field, CA 94035 Nathan Precup b and Eli Livne c University of Washington, Seattle, WA 98195 James Urnes, Sr. d Boeing Research & Technology, St. Louis, MO 63134 Eric Dickey e Boeing Research & Technology, Huntington Beach, CA Chester Nelson f Boeing Commercial Airplanes, WA 98124 Jonathan Chiew g Stanford University, Stanford, CA 94305 David L...
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ژورنال
عنوان ژورنال: International Journal of Aeroacoustics
سال: 2012
ISSN: 1475-472X,2048-4003
DOI: 10.1260/1475-472x.11.5-6.531