I have a bunch of data for a NACA 63-412 aerofoil which I want to use in my software. I have two data sets, one for reynolds number 400000 and one for 5000000. I need to interpolate/extrapolate the data so that I can calculate with other reynolds numbers. The furthest I have gotten now is this, I have drawn two lines from this data and now I need to connect those into i suppose a surface but really wouldn't know how? any help would be greatly appreciated!
Cd1 = [0.00880.00890.00890.0090.0090.0090.0090.0090.00910.00910.00920.00930.00940.00960.00980.01010.01060.01160.0133];Cl1= [-0.00530.05230.10960.16750.22480.28230.33920.39520.4520.50890.56470.62060.67670.73210.78580.8360.8850.9280.9606];RE1= [400000400000400000400000400000400000400000400000400000400000400000400000400000400000400000400000400000400000400000];Cd2 = [0.0080.0080.0080.00810.00810.00810.00810.00820.00820.00830.00840.00850.00870.00890.00930.01010.01120.01270.0141];Cl2 = [-0.00480.0530.11080.16890.22670.28370.34060.39820.4550.51170.56870.62490.6810.73560.78790.83520.87930.91720.9541];RE2 = [500000500000500000500000500000500000500000500000500000500000500000500000500000500000500000500000500000500000500000];figure(1)hold onplot3(Cl1,Cd1,RE1);plot3(Cl2,Cd2,RE2);
Best Answer