Assertion: airfoil's lift | /r/HasProperty | l
Facets:
Source sentences:
text: The lift per unit span (L') acting on a body in a two-dimensional inviscid flow field can be expressed as the product of the circulation Γ about the body, the fluid density ρ, and the speed of the body relative to the free-stream V.
text: If you know lift (L) and drag (D), calculate normal force (N) and axial force (A):