The pressure distribution of the naca0012 airfoil at zero angles of attack. airfoil equations can be found on the handout posted on blackboard or from online sources. compare its pressure distribution with the experimental data (find references) using a) 10, b) 20, and c) 100 panels equally distributed on both top and bottom side (that means twice the number of panels). comment on your results in the form of a report on

explanation:

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answer: jesus loves you

explanation:

answer:

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the equation above shows how temperature f, measured in degrees fahrenheit, relates to a temperature c, measured in degrees celsius. based on the equation, which of the following must be true?

a temperature increase of 1 degree fahrenheit is equivalent to a temperature increase of

5

9

degree celsius.

a temperature increase of 1 degree celsius is equivalent to a temperature increase of 1.8 degrees fahrenheit.

a temperature increase of

5

9

degree fahrenheit is equivalent to a temperature increase of 1 degree celsius.

a) i only

b) ii only

c) iii only

d) i and ii only