![photo](/responsive_image/150/150/0/0/0/cache/matlabcentral/profiles/17495523_1581328267396_DEF.jpg)
Turgut Ataseven
Followers: 0 Following: 0
Statistik
18 Fragen
0 Antworten
RANG
34.680
of 292.788
REPUTATION
1
BEITRÄGE
18 Fragen
0 Antworten
ANTWORTZUSTIMMUNG
61.11%
ERHALTENE STIMMEN
1
RANG
of 19.940
REPUTATION
N/A
DURCHSCHNITTLICHE BEWERTUNG
0.00
BEITRÄGE
0 Dateien
DOWNLOADS
0
ALL TIME DOWNLOADS
0
RANG
of 147.955
BEITRÄGE
0 Probleme
0 Lösungen
PUNKTESTAND
0
ANZAHL DER ABZEICHEN
0
BEITRÄGE
0 Beiträge
BEITRÄGE
0 Öffentlich Kanäle
DURCHSCHNITTLICHE BEWERTUNG
BEITRÄGE
0 Highlights
DURCHSCHNITTLICHE ANZAHL DER LIKES
Feeds
Frage
Runge-Kutta-4th-order solution of 3 ODEs
Hi. Lorenz equations are as follows: Parameter values: sigma = 10, b = 8/3, and r = 28. Employ initial conditions of x = y = ...
etwa ein Jahr vor | 2 Antworten | 1
2
AntwortenFrage
Getting same final value for various time-steps
Hi. I am trying to modify my Crank Nicholson method code so that it breaks when 14.9<T(11,11,k+1)<15.1 condition is satisfied. ...
etwa 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Index in position 3 exceeds array bounds (must not exceed 80000).
Hi. I am trying to modify my Crank Nicholson method code so that it breaks when 14.9<T(11,11,k+1)<15.1 condition is satisfied. ...
etwa 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Breaking loop at a desired value
Hi. I am trying to modify my FTSC methodd code so that it breaks when 14.9<T(11,11,k+1)<15.1 condition is satisfied. Since time...
etwa 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Time response of modes to an impulse
Hi. For a 4x4 plant matrix, I want to see the time response of short period mode and phugoid mode of an aircraft for an initial...
etwa 2 Jahre vor | 0 Antworten | 0
0
AntwortenFrage
Implementing the Trapezoidal Method
Hi. The aim is to utilize Trapezoidal Method for an integral with no variables, so we will get the x after integration. where ...
mehr als 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Out of memory error
Hi, please do not mind long lines because most of them are loops. Whenever I run the code, it runs for approximately fo...
mehr als 2 Jahre vor | 0 Antworten | 0
0
AntwortenFrage
Index in position 2 exceeds array bounds (must not exceed 1).
Hi. First of all sorry for asking the same question again and again but I am really close to the solution (probably). ...
mehr als 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Unable to perform assignment because the indices on the left side are not compatible with the size of the right side.
Hi. First of all sorry for asking the same question again and again but I am really close to the solution (probably). Ple...
mehr als 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Unable to perform assignment because the indices on the left side are not compatible with the size of the right side.
Hi. First of all sorry for asking the same question again and again but I am really close to the solution (probably). ...
mehr als 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Unable to perform assignment because the size of the left side is 1-by-1 and the size of the right side is 1-by-79201.
Hi. First of all sorry for asking the same question again and again but I am really close to the solution (maybe not). I have 2 ...
mehr als 2 Jahre vor | 0 Antworten | 0
0
AntwortenFrage
Utilizing the Euler Method
Hi. First of all sorry for asking a huge question.I need a guide to utilize the Euler Method. I am having troubles with the ...
mehr als 2 Jahre vor | 2 Antworten | 0
2
AntwortenFrage
Index exceeds the number of array elements (391).
Hi all. That is my function: function [Vtas_cl] = Velocities(H1,H2) Vcl_1 = 335; % Standard calibrated airspeed ...
mehr als 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Index exceeds the number of array elements (1).
Hi. My code tries to solve 6 ODEs with 6 state variables [horizontal position (x1 and x2), altitude (x3), the true airspeed (x4...
mehr als 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Too many input arguments.
Hi. My code tries to solve 6 ODEs with 6 state variables [horizontal position (x1 and x2), altitude (x3), the true airspeed ...
mehr als 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Cannot plot the full interval
function [] = FuelJetPlot H_climb = 0:500:35000; % Altitude [ft] for k1 = 1:length(H_climb) % CLIMB PHASE % Thru...
mehr als 2 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Not enough input arguments.
function yp = predprey(t,y,a,b,c,d) h=0.0625;tspan=[0 40];y0=[2 1]; a=1.2;b=0.6;c=0.8;d=0.3; yp = [a*y(1)-b*y(1)*y(2);-c*...
etwa 3 Jahre vor | 1 Antwort | 0
1
AntwortFrage
Not enough input arguments for bisection method function.
I have problems for determining variable "t" for "pCO2" value. This is the function of pH: function y = f(pH,pCO2) % F...
mehr als 3 Jahre vor | 1 Antwort | 0