leading edge of the wing is 1 inch, Main wing Rib height is 1.2 Inches, trailing edge is 0.9 inch, and chord length is 9 inches.
I am beginner.Please guide me.If any further Information is required you can may ask.
Dear Muhammad Ibtasam Khan
Cd=Fd/( 0.5 × 𝜌 × V2 × A)
Fd = the drag force , Cd = the drag coefficient, 𝜌= the mass density of the fluid, V = the flow speed of the object relative to the fluid, A = the reference area
Cl=Fl/( 0.5 × 𝜌 × V2 × S)
Fl = the lift force, Cl = is the lift coefficient , 𝜌= is the air density, V = is the velocity or true airspeed, S = is the planform wing area
HEllo there,
please visit the following link for more info
http://mypages.iit.edu/~vural/RC%20Airplane%20Design.pdf
Dear Muhammad Ibtasam Khan
Cd=Fd/( 0.5 × 𝜌 × V2 × A)
Fd = the drag force , Cd = the drag coefficient, 𝜌= the mass density of the fluid, V = the flow speed of the object relative to the fluid, A = the reference area
Cl=Fl/( 0.5 × 𝜌 × V2 × S)
Fl = the lift force, Cl = is the lift coefficient , 𝜌= is the air density, V = is the velocity or true airspeed, S = is the planform wing area
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