Project

Flow over BOEING 737 MID SPAN AIRFOIL b737b-il

The following data was colleted for BOEING 737 MID SPAN AIRFOIL(b737b-il)

The velocity chosen was 250 m/s at 101325 Pa and 293.3 K.

1) For angle of Attack 2 degrees:

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2) For angle of Attack 4 degrees:

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3) For angle of Attack 6 degrees:

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4) For angle of Attack 8 degrees:

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5) For angle of Attack 10 degrees:

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THE FOLLOWING TABLE COMPARES THE AVERAGE DRAG FORCE AND THE AVERAGE LIFT FORCE.

ANGLE OF ATTACK DRAG FORCE (N) LIFT FORCE (N)
2 41.494 514.678
4 87.514 1317.569
6 219.801 1967.218
8 352.521 2041.297
10 434.842 2060.782
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