Abstract
Nomenclature AR = aspect ratio, b=S b = span, mm CD = configuration drag coefficient CL = configuration lift coefficient c = chord, mm ds = angle of strake setting relative to wing chord plane (positive, strake leading edge up), q = freestream dynamic pressure, 1 2 1V 2 1, kPa Re = Reynolds number based on wing model chord, 1V1c= 1 S = reference area, m V1 = freestream velocity, m=s x, y, z = aerodynamic axes = angle of attack, deg = absolute viscosity, N s=m = air density, kg=m
Published Version
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a callDisclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.
