Considering both maximum lift coefficient and speed-range ratio CLmax CDmin, with flap neutral no appreciable improvement was found with use of more than single leading-edge slot.
Effect of multiple fixed slots and trailing-edge flap on lift and drag of Clark Y airfoil
Nat Advisory Committee Aeronautics -- Report
1932
8 pages
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Effects of equal-pressure fixed slots on characteristics of Clark Y airfoil
Engineering Index Backfile | 1934
|