Anyone able to find the error in this aerofoil code?
    3 vues (au cours des 30 derniers jours)
  
       Afficher commentaires plus anciens
    
if true
  %943639  %uvwxyz
%NACAwxyz %chord length z %u angle of attack
clc
%
NACA = string([4 4 7 4]);
L = length(NACA);
c = 3;
if L == 4
M = str2double(NACA(1))/100; % maximun chamber
P = str2double(NACA(2))/10; % maximun chamber along the cord
t1 = str2double(NACA(3));
t2 = str2double(NACA(4)); 
tmax =((10*t1+t2)/100)*(c/10); % max thickness
end
%%Mean Camber Line
x = linspace(0,c,1000);
N = P*c;
if 0<=x<=(P*c)
  dZdX = ((M*2)/P.^2)*(P-(x/c));
  Z = ((M*c)/P.^2)*(2*P*(x/c)-(x/c).^2);
elseif (P*c)<=x<=c
  dZdX = ((M*2)/(1-P).^2)*(P-(x/c));
  Z = ((M*c)/(1-P).^2)*((1-2*P)+2*P*(x/c)-(x/c).^2);
end
%%Equation for Upper and Lower Surface
%
Y = (tmax/0.2)*(0.2969*sqrt(x/c)-0.1281*(x/c)-0.3516*((x/c).^2)+0.2843*((x/c).^3)-0.1015*((x/c).^4));
%
theta = atan(dZdX); 
%
xup = x-Y*sin(theta);
yup = Z+Y*cos(theta);
xlow = x+Y*sin(theta);
ylow = Z-Y*cos(theta);
 fprintf("Printing Graph\n");
plot(xup,yup,'g'); hold on
plot(xlow,ylow,'g'); hold on
fprintf("\nPrinting Mean Camber Line");
plot(xup,Z,'b-.'); hold on
plot(0:3,0); hold on
axis([-0.5 3.5 -0.4 0.7])
 end
The Error is:
Error using * Inner matrix dimensions must agree.
Error in Aerofoil (line 33) xlow = x+Y*sin(theta);
Thank you
3 commentaires
  Jan
      
      
 le 12 Déc 2017
				
      Modifié(e) : Jan
      
      
 le 12 Déc 2017
  
			I assume this is more direct:
NACA = [4 4 7 4];
M  = NACA(1) / 100; % maximun chamber
P  = NACA(2) / 10;  % maximun chamber along the cord
t1 = NACA(3);
t2 = NACA(4);
While "the graph is wrong" has a meaning for you, the readers in the forum cannot imagine, what you expect. Please read: https://www.mathworks.com/matlabcentral/answers/6200-tutorial-how-to-ask-a-question-on-answers-and-get-a-fast-answer.
Réponses (1)
  Jan
      
      
 le 12 Déc 2017
        
      Modifié(e) : Jan
      
      
 le 12 Déc 2017
  
      if 0<=x<=(P*c)
This will most likely not do what you expect. Unfortunately there is no comment, which defines clearly, what the intention is. But I guess you want:
if 0<=x & x<=(P*c)
Note that "0<=x<=(P*c)" is evaluated from left to right: 0<=x is either TRUE or FALSE, which is treated as 1 or 0. In the next step you get "1<=P*c" or "0<=P*c".
The next problem is that x is a vector, but the condition of an if must be scalar. Therefore Matlab inserts this automatically:
if all(0<=x<=(P*c))
So you need either a for loop over all elements of x, or logical indexing:
index    = (0<=x & x<=P*c);
dZdX     = ((M*2)/P.^2)*(P-(x(index)/c));
Z(index) = ((M*c)/P.^2)*(2*P*(x(index)/c)-(x(index)/c).^2);
The same for "elseif (P*c)<=x<=c".
4 commentaires
  Jan
      
      
 le 12 Déc 2017
				
      Modifié(e) : Jan
      
      
 le 12 Déc 2017
  
			Z    = zeros(size(x));  % Or NaN(size(x)) ?
dZdX = zeros(size(x));  % Or NaN(size(x)) ?
index       = (0<=x & x<=P*c);
dZdX(index) = ((M*2)/P.^2)*(P-(x(index)/c));
Z(index)    = ((M*c)/P.^2)*(2*P*(x(index)/c)-(x(index)/c).^2);
index    = (P*c<=x & x<=c)
dZdX     = ((M*2)/(1-P).^2)*(P-(x(index)/c));
Z(index) = ((M*c)/(1-P).^2)*((1-2*P)+2*P*(x(index)/c)-(x(index)/c).^2);
The TRUE and FALSE values of the logical indexing replace the need for a loop and the IF branches.
Voir également
Catégories
				En savoir plus sur Gas Dynamics dans Help Center et File Exchange
			
	Community Treasure Hunt
Find the treasures in MATLAB Central and discover how the community can help you!
Start Hunting!


