User:Eas4200c.f08.wiki.d/HW7

Single Cell Airfoil
EDU>> NewAirfoil(2415,.5,[0 0 0])

Single Cell

q_0 =

2.9437e+004

q_hf =

2.9437e+004

q_fb =

-2.2512e+005

q_be =

3.2195e+004

q_eh =

2.8555e+005

Note: All values in N/m

Multi Cell Airfoil
EDU>> NewAirfoil(2415,.5,[0 0 0])

Multi Cell

q_1 =

3.2721e+004

q_2 =

2.6482e+004

q_3 =

3.7939e+004

q_hf =

3.7939e+004

q_fb =

-2.2807e+005

q_be =

3.5480e+004

q_eh =

2.8260e+005

q_w1 =

-6.2391e+003

q_w2 =

1.1456e+004

Note: All values in N/m

Also, it can be seen here that the shear flow values in the skin panels are similar between the single and multi cell cases. This verifies the validity of the two cases.