UDF code
1 Attachment(s)
How should I define two rotations for a moving wing?
This code only simulates the roll but when I add pitch the motion becomes completely wrong. #include "udf.h" #include "dynamesh_tools.h" real w, pi, Aroll, Apitch, roll, droll, pitch, dpitch, yaw, dyaw, frequency, T; real Ar, Ap, Ay; DEFINE_CG_MOTION(code, dt, v_cg, omega, time, dtime) { Thread *t; NV_S(v_cg, =, 0.0); NV_S(omega, =, 0.0); if (!Data_Valid_P()) { Message("Wrong\n"); return; } t=DT_THREAD((Dynamic_Thread*)dt); frequency = 3.0; pi = 3.141592654; /* define motion variables */ Ar = 30.0; /*roll amplitude*/ Ap = 5.0; /*pitch amplitude*/ Ay = 0.0; /*yaw amplitude*/ Aroll = Ar*pi/180.0; /*conversion to radians*/ Apitch = Ap*pi/180.0; /*conversion to radians*/ w=2.0*pi*frequency; /*omega (radians)*/ T=1.0/frequency; roll = Aroll*sin(w*time + pi/2); droll = w*Aroll*cos(w*time + pi/2); pitch = Apitch*sin(w*time+pi/2); dpitch = w*Apitch*cos(w*time+pi/2); /*euler angles initial frame mod 1*/ omega[0] = droll; omega[1] = 0; omega[2] = 0; Message("time:%f omegax:%f omegay:%f omegaz:%f \n", time, omega[0], omega[1],omega[2]); } 
Quote:
Make sure that the cg location is correct because rotation takes place about cg and not about the origin. 
It still doesn't work. The problem is that when I use roll or pitch separately the wing motion is ok but when I consider both of them simultaneously the motion becomes wrong.

t=DT_THREAD((Dynamic_Thread*)dt);
I found error in line 21 (t=DT_THREAD((Dynamic_Thread*)dt);) Can any one find solution to this.My problem is 2D and i m applying only rolling motion. 
Aerofoil rolling UDF
Structure reference is not implemented is error showing in line21( posted previously)

All times are GMT 4. The time now is 19:46. 