...13.39066267
22.05520949
31.60227434
35.89970274
39.23440003
50.30038346
61.72612467
73.51958827
88.75778292
112.1136364
119.6581416
134.0316193
next the structure should be submit to lateral force 150*sin(f*t).the author indicate that natural frequency is 12.69 Why I have 15 valus, thanks for...
I m trying to resolve a problem of simple portale frame restrained at base were each bar is descritized to 4 element (11 node X 3ddl=33 subject to dynamic load, so we can reduce the problem if the bar have just 2 node in this case with the two restrained node at base we can reduce the problem to...
...system M(22,22)which is the sum off all consistent mass matrix of the structure.To obtain the natural frequency i uses this code:
Z=(inv(M))*K;
[V,D]=eig(Z);
Omega=(sqrt(diag(D)));
Freq=((Omega))/(2*pi);
I get Warning: Matrix is close to singular or badly scaled. Results may be inaccurate...
sorry for the link
the new link containing the pdf (kawashima_dynamic experiment of portal frame) and ([M],[C],[K]) results finally the function Rajasteran
to obtain natural frequency all are in the folder in the link bellow:
the first question:in the mass matrix the area A is not indicate in the doccument or in any other document I found in the net
second :My results are given in folder system ([M],[C],[K])
I use to resolve it this code RAJESKARAN(folder system)
but the results are not conform
Thanks to help
Sorry,for the misunderstanding and for ma bade language.
and i will try to explain my problem better:
I try to verify the experimental results (natural frequency of simple portale frame with semi rigid joint) obtained par SUKEO KAWASffiMA
I m a new user of matlab and i have a question about how to obtain natural frequency and mode shape corresponding in the general case of system mass,sitiffness and viscous dumpinig (MDOF)
Example:
m=[40000 4000 0;0 30000 0;50000 0 20000];
c=[330 0 0;0 -8000 8000;0 -8000 8000];
k=[30000...
can somme one help me to resolve using matlab a dynamic system of diferentiel equation representing the dynamic behavior of frame structure(the matrix system is obtained by using finite element method)
thanks
sorry for the attached file and thanks for the linkhttp://files.engineering.com/getfile.aspx?folder=ece8974f-562b-4e02-bcfe-3f12c3bc480d&file=SECANT_STIFFNESS_BIEN_DEFINI.pdf
I'm trying to develop a computer program to analysis frame including p-delta effect using secant stiffness method but i have problems to understand the procedure mentioned in the attached file
1.Set up the member stiffness matrices for all members and assemble them in structure stiffness matrix...