Consider an naca 2412 airfoil in a low-speed fl ow at zero degrees angle of attack and a reynolds number of 8.9 × 10 6 . calculate the percentage of drag from pressure drag due to fl ow separation (form drag). assume a fully turbulent boundary layer over the airfoil. assume that the airfoil is thin enough that the skin-friction drag can be estimated by the fl at-plate results discussed in ch. 4.

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i lost in getting someone back.

i learned that people are really two-faced and no matter how angelic someone appears they always have a devil side and that you cant trust anyone anymore no matter how dear they are to you.

if your wondering who it waz it waz mah still miss her tho

~batmans wife dun dun

answer:

an example of solubility is salt or sugar dissolving in water.

rate as brainliest plz

answer:

the formula for amps is watts divided by volts. to use the chart, cover up the a with your finger and use the remaining chart calculation of w divided by v. using our sample panel data, 60 watts divided by 12 volts equals 5 amps.

explanation: