A NACA 2412 airfoil with a chord of 0.64m is flying in an airstream of standard sea level conditions. The freestream velocity is 70 m/s. Given the lift per unit span is 1,254 N/m. By using the experimental data for NACA 2412 data plot in Figure Q1c, investigatethe angle of attack of the airfoil and the analyze the value of drag per unit spanof the airfoil. Given that at standard sea level, ?=1.789×10-5 kg/m.s

Elements Of Electromagnetics
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A NACA 2412 airfoil with a chord of 0.64m is flying in an airstream of standard sea level conditions. The freestream velocity is 70 m/s. Given the lift per unit span is 1,254 N/m. By using the experimental data for NACA 2412 data plot in Figure Q1c, investigatethe angle of attack of the airfoil and the analyze the value of drag per unit spanof the airfoil. Given that at standard sea level, ?=1.789×10-5 kg/m.s.

0.024
NACA 2412 anfal
0.020
-Eg 4.7)
n 20
0016
1.6-
0.012
1-2-
0.008
Lit culicient
corfisient
0.004
-0.05
0.4
E (44)
Mornent
coetficient
Woment
-0.1
-02
• Re-31X 10
a Re-8,9 X 10
-0.15
-03
B Re- 89X 10
04
-*0 8 15 24
-12 -8
12 16
agees
deces
Figure Q1(c)
Transcribed Image Text:0.024 NACA 2412 anfal 0.020 -Eg 4.7) n 20 0016 1.6- 0.012 1-2- 0.008 Lit culicient corfisient 0.004 -0.05 0.4 E (44) Mornent coetficient Woment -0.1 -02 • Re-31X 10 a Re-8,9 X 10 -0.15 -03 B Re- 89X 10 04 -*0 8 15 24 -12 -8 12 16 agees deces Figure Q1(c)
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