Assertion: fuselage's section | /r/CapableOf | stall at angles of attack
Facets:
Source sentences:
text: Most airfoil sections stall at angles of attack about 16°, although an actual wing having the same profile may stall at a slightly different value (often about 18°) due to its geometry and interaction with the fuselage.
text: Most airfoil sections stall at angles of attack about 16°, although an actual wing having the same profile may stall at a slightly different value (often about 18°) due to its geometry and interaction with the fuselage.