Assertion: airfoil's ratio | /r/HasProperty | varied by location of the discontinuity
Facets:
value: with reference to the trailing edge
type: OTHER
value: according to aerodynamic characteristics
type: CAUSE
value: (step)
type: OTHER
Source sentences:
text: Also, the ratio of the upper or camber surface area at 84 to the under surface area at 94 of the wedge portion (always greater than unity) can be varied by location of the discontinuity (step) with reference to the trailing edge, according to aerodynamic characteristics desired.