Assertion: airfoil's thickness | /r/HasProperty | 12%
Facets:
Source sentences:
text: Following a dash, the first digit indicates the design lift coefficient in tenths (0.2) and the final two digits specify the maximum thickness in tenths of chord (12%).
text: Then the effects of the relative thickness of airfoil on aerodynamic performance are explored, using the above numerical method, by simulating flows around airfoils of different relative thicknesses (12%, 14%, 16%, 18%), as well as different locations of the maximum relative thickness (x/c = 22%, 26%, 30%, 34%), at a low Reynolds number of 5 × 105.
text: The final two digits specify the thickness in percentage of chord, 12%.