Induced drag is a function of angle of attack, and varies with AoA and the lift the airfoil is producing. Induced drag is produced when lift is produced, but isn't a function of lift; it's a function of AoA. At a minimal AoA or a negative AoA, the value of induced drag is considerably lessened, though not completely eliminated.
Likewise, parastic drag is also affected by the surface exposed to the slipstream, and in an unloaded or zero G condition, while no specific change in EAS or TAS may occur, the exposed wetted or flat plate area, as well as what is actually exposed to the slipstream, may change substantially, resulting in chages in parasitic drag
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