NDLI: Effects of leading-edge bevel angle on the aerodynamic forces of a non-slender 50° delta wing

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Effects of leading-edge bevel angle on the aerodynamic forces of a non-slender 50° delta wing

Content Provider	Scilit
Author	Wang, J. J. Lu, S. F.
Copyright Year	2005
Description	The aerodynamic performances of a non-slender 50° delta wing with various leading-edge bevels were measured in a low speed wind tunnel. It is found that the delta wing with leading-edge bevelled leeward can improve the maximum lift coefficient and maximum lift to drag ratio, and the stall angle of the wing is also delayed. In comparison with the blunt leading-edge wing, the increment of maximum lift to drag ratio is 200%, 98% and 100% for the wings with relative thickness t/c = 2%, t/c = 6.7% and t/c = 10%, respectively.
Related Links	https://www.cambridge.org/core/services/aop-cambridge-core/content/view/F4659DA7C33FB95543F31A684E53988D/S0001924000000828a.pdf/div-class-title-effects-of-leading-edge-bevel-angle-on-the-aerodynamic-forces-of-a-non-slender-50-delta-wing-div.pdf
Ending Page	407
Page Count	5
Starting Page	403
ISSN	00019240
e-ISSN	20596464
DOI	10.1017/s0001924000000828
Journal	The Aeronautical Journal
Issue Number	1098
Volume Number	109
Language	English
Publisher	Cambridge University Press (CUP)
Publisher Date	2005-08-01
Access Restriction	Open
Subject Keyword	The Aeronautical Journal Aerospace Engineering
Content Type	Text
Resource Type	Article
Subject	Aerospace Engineering

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