Wedge concept integrated into basic airfoil design. Current airfoil design, DLBA 238, developed to produce airfoil with superior geometric characteristics and equivalent cruise aerodynamic characteristics. "Trailing-edge wedge" concept improved by integration into basic airfoil design for DLBA 238. Trailing-edge thickness and maximum thickness constrained to be same as baseline DLBA 032. Base drag-penalty of wedge avoided. Airfoil upper-surface geometry held fixed.
Divergent-Trailing-Edge Airfoil
NASA Tech Briefs ; 12 , 8
1988-09-01
Sonstige
Keine Angabe
Englisch
Divergent-Trailing-Edge Airfoil Flow
Online Contents | 1996
|Divergent-trailing-edge airfoil flow
AIAA | 1996
|"Measurements on a Divergent Trailing-Edge Airfoil"
British Library Conference Proceedings | 1999
|Drag Force Balance of a Blunt and Divergent Trailing-Edge Airfoil
Online Contents | 2010
|Three-dimensional wake dynamics of a blunt and divergent trailing edge airfoil
Tema Archiv | 2008
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