Assertion: airfoil's lift | /r/HasProperty | aoa of the stab
Facets:
Source sentences:
text: Since the wing has substantially more camber than the stab, the zero lift AOA of the wing is more negative than the zero lift AOA of the stab, by something approaching that 1.5 degrees.
text: Since the wing has substantially more camber than the stab, the zero lift AOA of the wing is more negative than the zero lift AOA of the stab, by something approaching that 1.5 degrees.