vja
Mechanical
- Apr 13, 2012
- 27
Hello everyone
I am use analysis--measure bodies to get center of mass of a tapered body.
Its a multibody part.
In the information file,it gives me the values and error estimates.
The error estimates values are in thousands which made me approach this forum...
============================================================
Date : 4/13/2012 9:47:54 AM
============================================================
Measurement Mass Properties
Displayed Mass Property Values
Volume = 67858.10989569816 in^3
Area = 229256.34693012343 in^2
Mass = 19197.05928949301 lbm
Weight = 19197.05928949301 lbf
Radius of Gyration = 268.23425597988 in
Centroid = 0.00000006766, 409.14083502539, 5.08644062443 in
============================================================
Detailed Mass Properties
Analysis calculated using accuracy of 0.99000000000
Information Units lbm - in
Density = 0.28290000000
Volume = 67858.10989569816
Area = 229256.34693012343
Mass = 19197.05928949301
First Moments
Mx, My, Mz = 0.00129887103, 7854300.86773500030, 97644.70223961631
Center of Mass
Xcbar, Ycbar, Zcbar = 0.00000006766, 409.14083502539, 5.08644062443
Moments of Inertia (WCS)
Ix, Iy, Iz = 4594076121.81324480000, 4728866.71545003540, 4591660862.09269330000
Moments of Inertia (Centroidal)
Ixc, Iyc, Izc = 1380064242.26730700000, 4232202.73521834610, 1378145646.52698730000
Moments of Inertia (Spherical)
I = 1381221045.76475620000
Products of Inertia (WCS)
Iyz, Ixz, Ixy = 57074532.32435357600, 0.37765596938, 0.46118485916
Products of Inertia (Centroidal)
Iyzc, Ixzc, Ixyc = 17124097.31423184600, 0.37104933899, -0.07023632060
Radii of Gyration (WCS)
Rx, Ry, Rz = 489.19469685695, 15.69499507060, 489.06608693092
Radii of Gyration (Centroidal)
Rxc, Ryc, Rzc = 268.12190635878, 14.84792888050, 267.93546704505
Radii of Gyration (Spherical)
R = 268.23425597988
Principal Axes (Direction vectors relative to the WCS)
Xp(X), Xp(Y), Xp(Z) = 1.00000000000, 0.00000000277, -0.00000021808
Yp(X), Yp(Y), Yp(Z) = 0.00000021810, -0.01246083498, 0.99992236078
Zp(X), Zp(Y), Zp(Z) = 0.00000000005, -0.99992236078, -0.01246083498
Principal Moments
I1, I2, I3 = 1380064242.26730700000, 1378359043.64586830000, 4018805.61633741950
============================================================
Error Estimates
Volume = 37.47378610535
Area = 1.70501403591
Mass = 10.60133408920
Moments of Inertia (Spherical) = 0.45207876192
Center of Mass = 8683.37543481869, 13020.81411574129, 8737.29849048585
Moments of Inertia (WCS) = 29544060.32917690300, 20663990.09437890400, 29455451.10679721800
Products of Inertia (WCS) = 17010880.68397417700, 16944651.08697374900, 20519436.68664599600
Anyhow I will be using the cg values in my calculations.
Your help is appreciated.
thanks
I am use analysis--measure bodies to get center of mass of a tapered body.
Its a multibody part.
In the information file,it gives me the values and error estimates.
The error estimates values are in thousands which made me approach this forum...
============================================================
Date : 4/13/2012 9:47:54 AM
============================================================
Measurement Mass Properties
Displayed Mass Property Values
Volume = 67858.10989569816 in^3
Area = 229256.34693012343 in^2
Mass = 19197.05928949301 lbm
Weight = 19197.05928949301 lbf
Radius of Gyration = 268.23425597988 in
Centroid = 0.00000006766, 409.14083502539, 5.08644062443 in
============================================================
Detailed Mass Properties
Analysis calculated using accuracy of 0.99000000000
Information Units lbm - in
Density = 0.28290000000
Volume = 67858.10989569816
Area = 229256.34693012343
Mass = 19197.05928949301
First Moments
Mx, My, Mz = 0.00129887103, 7854300.86773500030, 97644.70223961631
Center of Mass
Xcbar, Ycbar, Zcbar = 0.00000006766, 409.14083502539, 5.08644062443
Moments of Inertia (WCS)
Ix, Iy, Iz = 4594076121.81324480000, 4728866.71545003540, 4591660862.09269330000
Moments of Inertia (Centroidal)
Ixc, Iyc, Izc = 1380064242.26730700000, 4232202.73521834610, 1378145646.52698730000
Moments of Inertia (Spherical)
I = 1381221045.76475620000
Products of Inertia (WCS)
Iyz, Ixz, Ixy = 57074532.32435357600, 0.37765596938, 0.46118485916
Products of Inertia (Centroidal)
Iyzc, Ixzc, Ixyc = 17124097.31423184600, 0.37104933899, -0.07023632060
Radii of Gyration (WCS)
Rx, Ry, Rz = 489.19469685695, 15.69499507060, 489.06608693092
Radii of Gyration (Centroidal)
Rxc, Ryc, Rzc = 268.12190635878, 14.84792888050, 267.93546704505
Radii of Gyration (Spherical)
R = 268.23425597988
Principal Axes (Direction vectors relative to the WCS)
Xp(X), Xp(Y), Xp(Z) = 1.00000000000, 0.00000000277, -0.00000021808
Yp(X), Yp(Y), Yp(Z) = 0.00000021810, -0.01246083498, 0.99992236078
Zp(X), Zp(Y), Zp(Z) = 0.00000000005, -0.99992236078, -0.01246083498
Principal Moments
I1, I2, I3 = 1380064242.26730700000, 1378359043.64586830000, 4018805.61633741950
============================================================
Error Estimates
Volume = 37.47378610535
Area = 1.70501403591
Mass = 10.60133408920
Moments of Inertia (Spherical) = 0.45207876192
Center of Mass = 8683.37543481869, 13020.81411574129, 8737.29849048585
Moments of Inertia (WCS) = 29544060.32917690300, 20663990.09437890400, 29455451.10679721800
Products of Inertia (WCS) = 17010880.68397417700, 16944651.08697374900, 20519436.68664599600
Anyhow I will be using the cg values in my calculations.
Your help is appreciated.
thanks