I'll give you the benefit of the doubt and assume you're being pedantic, but here's a picture anyway...
Top one will produce a force if it's rotated relative to the oncoming air. Presumably at the expense of significant drag. Any difference in pressure is a consequence.
Bottom one will generate lift at a neutral angle to the airflow, with minimal drag. Difference in pressure is deliberate.
The symmetrical aerofoil produces no lift at neutral AoA, but it produces lift in the same way as the cambered one does at a positive AoA. It’s not about air molecules smashing into the lower surface (just use a flat plate in that case), it’s lift due to pressure differential.
I'll give you the benefit of the doubt and assume you're being pedantic, but here's a picture anyway...
Top one will produce a force if it's rotated relative to the oncoming air. Presumably at the expense of significant drag. Any difference in pressure is a consequence.
Bottom one will generate lift at a neutral angle to the airflow, with minimal drag. Difference in pressure is deliberate.