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Uthibitishaji kwa modeli ya umbo rahisi

Uchambuzi tuli wa elastiki

Uthibitishaji huu unatumia cantilever beam iliyogawanywa kuwa mesh kama inavyoonyeshwa katika Kielelezo 9.1.1. Uchambuzi ulifanywa kwa masharti saba, exA hadi exG, kwa kubadilisha masharti ya mzigo kama inavyoonyeshwa katika Kielelezo 9.1.2. Kesi exG ina masharti sawa ya mzigo na exA, lakini ni kesi ya uthibitishaji inayotumia solver ya mbinu ya moja kwa moja.

Matokeo ya uthibitishaji kwa kila kesi yanaonyeshwa katika Jedwali 9.1.1 hadi Jedwali 9.1.7.

Mfano wa mesh ya cantilever beam (elementi za hexahedral) Kielelezo 9.1.1 Mfano wa mesh ya cantilever beam (elementi za hexahedral)

(a) exA,G: Mzigo uliokolezwa
(b) exD: Mvuto
(c) exB: Mzigo uliosambazwa kwenye uso
(d) exE: Nguvu ya centrifugal
(e) exC: Mzigo wa ujazo
(f) exF: Mzigo wa joto
Kipengee Thamani
Moduli ya Young \(E = 4000.0\ kgf/mm^2\)
Urefu \(L = 10.0\ mm\)
Uwiano wa Poisson \(\nu = 0.3\)
Eneo la sehemu ya msalaba \(A = 1.0\ mm^2\)
Msongamano wa misa \(\rho = 8.0102 x 10^{-10}\ kg\,s^2/mm^4\)
Moment ya pili ya eneo \(I = 1.0/12.0\ mm^4\)
Uharakishaji wa mvuto \(g = 9800.0\ mm/s^2\)
Mgawo wa upanuzi wa joto wa mstari \(\alpha = 1.0 \times 10^{-5}\)
Jedwali 9.1.2 Masharti ya uthibitishaji wa modeli ya cantilever beam
Jedwali 9.1.1 exA: Matokeo ya uthibitishaji wa tatizo la mzigo uliokolezwa
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: \(\delta_{max}= -1.000\) Maelezo
NASTRAN programu ya kibiashara FrontISTR
A231 40 -0.338 -0.371 -0.371 33nodi / tatizo la plane stress
A232 40 -0.942 -1.002 -1.002 105nodi / tatizo la plane stress
A241 20 -0.720 -0.711 -0.711 33nodi / tatizo la plane stress
A242 20 -0.910 -1.002 -1.002 85nodi / tatizo la plane stress
A341 240 -0.384 -0.384 -0.386 99nodi
A342 240 -0.990 -0.990 -0.999 525nodi
A351 80 -0.353 -0.355 -0.351 99nodi
A352 80 -0.993 -0.993 -0.992 381nodi
A361 40 -0.954 -0.985 -0.984 99nodi
A362 40 -0.994 -0.993 -0.993 220nodi
A731 40 - - -0.991 33nodi / mbinu ya moja kwa moja
A741 20 - - -0.996 33nodi / mbinu ya moja kwa moja
Jedwali 9.1.2 exB: Matokeo ya uthibitishaji wa tatizo la mzigo uliosambazwa kwenye uso
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: \(\delta_{max}= -3.750\) Maelezo
NASTRAN programu ya kibiashara FrontISTR
B231 40 -1.281 -1.403 -1.403 33nodi / tatizo la plane stress
B232 40 -3.579 -3.763 -3.763 105nodi / tatizo la plane stress
B241 20 -3.198 -2.680 -2.680 33nodi / tatizo la plane stress
B242 20 -3.426 -3.765 -3.765 85nodi / tatizo la plane stress
B341 240 -1.088 -1.449 -1.454 99nodi
B342 240 -3.704 -3.704 -3.748 525nodi
B351 80 -3.547 -1.338 -1.325 99nodi
B352 80 -0.3717 -3.716 -3.713 381nodi
B361 40 -3.557 -3.691 -3.688 99nodi
B362 40 -3.726 -3.717 -3.717 220nodi
B731 40 - - -3.722 33nodi / mbinu ya moja kwa moja
B741 20 - - -3.743 33nodi / mbinu ya moja kwa moja
Jedwali 9.1.3 exC: Matokeo ya uthibitishaji wa tatizo la mzigo wa ujazo
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: \(\delta_{max}= -2.944^{-5}\) Maelezo
NASTRAN programu ya kibiashara FrontISTR
C231 40 - -1.101e-5 -1.101e-5 33nodi / tatizo la plane stress
C232 40 - -2.951e-5 -2.951e-5 105nodi / tatizo la plane stress
C241 20 - -2.102e-5 -2.102e-5 33nodi / tatizo la plane stress
C242 20 - -2.953e-5 -2.953e-5 85nodi / tatizo la plane stress
C341 240 - -1.136e-5 -1.140e-5 99nodi
C342 240 - -2.905e-5 -2.937e-5 525nodi
C351 80 - -1.050e-5 -1.039e-5 99nodi
C352 80 - -2.914e-5 -2.911e-5 381nodi
C361 40 - -2.895e-5 -2.893e-5 99nodi
C362 40 - -2.915e-5 -2.915e-5 220nodi
C731 40 - - -2.922e-5 33nodi / mbinu ya moja kwa moja
C741 20 - - -2.938e-5 33nodi / mbinu ya moja kwa moja
Jedwali 9.1.4 exD: Matokeo ya uthibitishaji wa tatizo la mvuto
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: \(\delta_{max}= -2.944^{-5}\) Maelezo
NASTRAN programu ya kibiashara FrontISTR
D231 40 -1.101e-5 -1.101e-5 -1.101e-5 33nodi / tatizo la plane stress
D232 40 -2.805e-5 -2.951e-5 -2.951e-5 105nodi / tatizo la plane stress
D241 20 -2.508e-5 -2.102e-5 -2.102e-5 33nodi / tatizo la plane stress
D242 20 -2.684e-5 -2.953e-5 -2.953e-5 85nodi / tatizo la plane stress
D341 240 -1.172e-5 -1.136e-5 -1.140e-5 99nodi
D342 240 -2.906e-5 -2.905e-5 -2.937e-5 525nodi
D351 80 -1.046e-5 -1.050e-5 -1.039e-5 99nodi
D352 80 -2.917e-5 -2.914e-5 -2.911e-5 381nodi
D361 40 -2.800e-5 -2.895e-5 -2.893e-5 99nodi
D362 40 -2.919e-5 -2.915e-5 -2.915e-5 220nodi
D731 40 - - -2.922e-5 33nodi / mbinu ya moja kwa moja
D741 20 - - -2.938e-5 33nodi / mbinu ya moja kwa moja
Jedwali 9.1.5 exE: Matokeo ya uthibitishaji wa tatizo la nguvu ya centrifugal
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: \(\delta_{max}= 2.635^{-3}\) Maelezo
NASTRAN programu ya kibiashara FrontISTR
E231 40 2.410e-3 2.616e-3 2.650e-3 33nodi / tatizo la plane stress
E232 40 2.447e-3 2.627e-3 2.628e-3 105nodi / tatizo la plane stress
E241 20 2.386e-3 2.622e-3 2.624e-3 33nodi / tatizo la plane stress
E242 20 2.387e-3 2.627e-3 2.629e-3 85nodi / tatizo la plane stress
E341 240 2.708e-3 2.579e-3 2.625e-3 99nodi
E342 240 2.639e-3 2.614e-3 2.638e-3 525nodi
E351 80 2.642e-3 2.598e-3 2.625e-3 99nodi
E352 80 2.664e-3 2.617e-3 2.616e-3 381nodi
E361 40 2.611e-3 2.603e-3 2.603e-3 99nodi
E362 40 2.623e-3 2.616e-3 2.616e-3 220nodi
E731 40 - - 2.619e-3 33nodi / mbinu ya moja kwa moja
E741 20 - - 2.622e-3 33nodi / mbinu ya moja kwa moja
Jedwali 9.1.6 exF: Matokeo ya uthibitishaji wa tatizo la mzigo wa thermal stress
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: \(\delta_{max}= 1.000^{-2}\) Maelezo
NASTRAN programu ya kibiashara FrontISTR
F231 40 - 1.016e-2 1.007e-2 33nodi / tatizo la plane stress
F232 40 - 1.007e-2 1.007e-2 105nodi / tatizo la plane stress
F241 20 - 1.010e-2 1.010e-2 33nodi / tatizo la plane stress
F242 20 - 1.006e-2 1.006e-2 85nodi / tatizo la plane stress
F341 240 - 1.047e-2 1.083e-2 99nodi
F342 240 - 1.018e-2 1.022e-2 525nodi
F351 80 - 1.031e-2 1.062e-2 99nodi
F352 80 - 1.015e-2 1.017e-2 381nodi
F361 40 - 1.026e-2 1.026e-2 99nodi
F362 40 - 1.016e-2 1.016e-2 220nodi
Jedwali 9.1.7 exG: Matokeo ya uthibitishaji wa mbinu ya moja kwa moja (tatizo la mzigo uliokolezwa)
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: δmax= -1.000 Maelezo
NASTRAN programu ya kibiashara FrontISTR
G231 40 -0.338 -0.371 -0.371 33nodi / tatizo la plane stress
G232 40 -0.942 -1.002 -1.002 105nodi / tatizo la plane stress
G241 20 -0.720 -0.711 -0.711 33nodi / tatizo la plane stress
G242 20 -0.910 -1.002 -1.002 85nodi / tatizo la plane stress
G341 240 -0.384 -0.384 -0.386 99nodi
G342 240 -0.990 -0.990 -0.999 525nodi
G351 80 -0.353 -0.355 -0.351 99nodi
G352 80 -0.993 -0.993 -0.992 381nodi
G361 40 -0.954 -0.985 -0.984 99nodi
G362 40 -0.994 -0.993 -0.993 220nodi
G731 40 - - -0.991 33nodi / mbinu ya moja kwa moja
G741 20 - - -0.996 33nodi / mbinu ya moja kwa moja

Uchambuzi tuli usio wa mstari

(2-1) exnl1: Uchambuzi usio wa mstari wa kijiometri

Modeli ya uthibitishaji ya kesi exI ni sawa na modeli za kesi exA hadi exG. Kielelezo 9.1.3 kinaonyesha mchoro wa dhana wa modeli ya uthibitishaji. Uchambuzi usio wa mstari wa kijiometri unafanywa kwa modeli hii. Matokeo ya uthibitishaji yanaonyeshwa katika Jedwali 9.1.8.

Hesabu isiyo ya mstari hutumia hatua 10 za mzigo, kila moja ikiwa na nyongeza ya mzigo 0.1P, hadi mzigo wa mwisho wa 1.0P.

Modeli ya uthibitishaji Kielelezo 9.1.3 Modeli ya uthibitishaji

Jedwali 9.1.8 exI: Matokeo ya uthibitishaji (historia ya maximum deflection)
Jina la kesi 0.1 0.2 0.3 0.4 0.5 0.6 0.7 0.8 0.9 1.0 Suluhisho la mstari
I231 - - - - - - - - - - -
I232 - - - - - - - - - - -
I241 - - - - - - - - - - -
I242 - - - - - - - - - - -
I341 0.039 0.077 0.116 0.154 0.193 0.232 0.270 0.309 0.348 0.386 0.386
I342 0.099 0.200 0.300 0.400 0.499 0.599 0.698 0.797 0.896 0.995 0.999
I351 0.035 0.070 0.105 0.141 0.176 0.211 0.246 0.281 0.316 0.351 0.351
I352 0.099 0.198 0.298 0.397 0.496 0.595 0.693 0.792 0.890 0.987 0.992
I361 0.070 0.139 0.209 0.278 0.348 0.417 0.487 0.556 0.625 0.694 0.984
I362 0.099 0.197 0.298 0.397 0.496 0.595 0.694 0.793 0.891 0.988 0.993

(2-2)  exnl2: Uchambuzi wa deformation ya elastoplastic

Tatizo hili la uthibitishaji linategemea National Agency for Finite Element Methods and Standards (U.K.): Test NL1 from NAFEMS, na hufanya uchambuzi wa deformation ya elastoplastic unaojumuisha geometric nonlinearity na sheria nyingi za hardening. Kielelezo 9.1.4 kinaonyesha modeli ya uchambuzi.

Modeli ya uchambuzi wa deformation ya elastoplastic

Kielelezo9.1.4 Modeli ya uchambuzi wa deformation ya elastoplastic

(1) Masharti ya uthibitishaji

Kipengee Thamani
Nyenzo Nyenzo elastoplastic ya Mises
Moduli ya Young \(E = 250 GPa\)
Uwiano wa Poisson \(\nu=0.25\)
Mkazo wa awali wa yield \(5 MPa\)
Strain ya awali ya yield \(0.25\times10^{-4}\)
Mgawo wa isotropic hardening \(H_i = 0\) au \(62.5 GPa\)

(2) Masharti ya mpaka

Kipengee Masharti ya mpaka Thamani
Hatua 1 Prescribed displacement kwenye nodi 2 na 3 \(u_x = 0.2500031251 * 10^{-4}\)
Hatua 2 Prescribed displacement kwenye nodi 2 na 3 \(u_x = 0.25000937518 * 10^{-4}\)
Hatua 3 Prescribed displacement kwenye nodi 3 na 4 \(u_y = 0.2500031251 * 10^{-4}\)
Hatua 4 Prescribed displacement kwenye nodi 3 na 4 \(u_y = 0.25000937518 * 10^{-4}\)
Hatua 5 Prescribed displacement kwenye nodi 2 na 3 \(u_x = -0.25000937518 * 10^{-4}\)
Hatua 6 Prescribed displacement kwenye nodi 2 na 3 \(u_x = -0.2500031251 * 10^{-4}\)
Hatua 7 Prescribed displacement kwenye nodi 3 na 4 \(u_y = -0.25000937518 * 10^{-4}\)
Hatua 8 Prescribed displacement kwenye nodi 3 na 4 \(u_y = -0.2500031251 * 10^{-4}\)

Nodi zote ambazo hazijaonyeshwa hapa zimezuiliwa kikamilifu. Suluhisho la kinadharia la tatizo hili ni kama ifuatavyo.

Strain (\(\times10^{-4}\))
[\(\varepsilon_x\), \(\varepsilon_y\), \(\varepsilon_z\)]
Mkazo sawa(\(MPa\))
[\(H_i=0\ H_k=0\); \(H_i=62.5\ H_k=0\)]
0.25, 0, 0 5.0; 5.0
0.50, 0, 0 5.0; 5.862
0.50, 0.25, 0 5.0; 5.482
0.50, 0.50, 0 5.0; 6.362
0.25, 0.50, 0 5.0; 6.640
0, 0.50, 0 5.0; 7.322
0, 0.25, 0 3.917; 4.230
0, 0, 0 5.0; 5.673

Kwa kulinganisha, matokeo ya hesabu ni kama ifuatavyo.

Strain (\(\times10^{-4}\))
[\(\varepsilon_x\), \(\varepsilon_y\), \(\varepsilon_z\)]
Mkazo sawa(\(MPa\)
[\(H_i=0\ H_k=0\); \(H_i=62.5\ H_k=0\)])
\(\varepsilon_{x}\) \(\varepsilon_{y}\)
0.25, 0, 0 5.0 (0.0%); 5.0 (0.0%)
0.50, 0, 0 5.0 (0.0%); 5.862 (0.0%)
0.50, 0.25, 0 5.0 (0.0%); 5.482 (0.0%)
0.50, 0.50, 0 5.0 (0.0%); 6.362 (-0.05%)
0.25, 0.50, 0 5.0 (0.0%); 6.640 (-0.21%)
0, 0.50, 0 5.0 (0.0%); 7.322 (-0.34%)
0, 0.25, 0 3.824 (-2.4%); 4.230 (-2.70%)
0, 0, 0 5.0 (0.0%); 5.673 (5.673 (-2.50%)

Uchambuzi wa contact(1)

Tatizo hili la uthibitishaji linategemea National Agency for Finite Element Methods and Standards (U.K.): tatizo la contact patch test CGS-4, na hujaribu uwezo wa finite-sliding contact wenye friction. Kielelezo 9.1.5 kinaonyesha modeli ya uchambuzi.

Modeli ya uchambuzi wa contact

Kielelezo9.1.5 Modeli ya uchambuzi wa contact

Sharti la usawa la tatizo hili ni kama ifuatavyo.

\[ Fcos\alpha - Gsin\alpha = \pm f_{c} \]

Katika hatua ya sticking friction, nguvu ya friction ni [ f_{c} = E_{t}\text{Δu} ] na katika hatua ya sliding friction ni [ f_{c} = \mu(G \cos \alpha + F \sin \alpha) ] .

Ulinganisho kati ya matokeo ya hesabu na suluhisho la uchambuzi ni kama ifuatavyo.

\(\mu\) Suluhisho la uchambuzi \(F/G\) Matokeo ya hesabu \(F/G\)
0.0 0.1 0.1
0.1 0.202 0.202
0.2 0.306 0.306
0.3 0.412 0.412

Uchambuzi wa contact(2): Tatizo la Hertz contact

Uthibitishaji huu unachambua tatizo la Hertz contact kati ya silinda yenye urefu usio na kikomo na plane isiyo na kikomo. Radius ya silinda ni R=8mm, na Moduli ya Young E pamoja na uwiano wa Poisson µ wa mwili unaodeform ni 1100Mpa na 0.0, mtawalia. Eneo la contact linadhaniwa kuwa dogo vya kutosha ukilinganisha na radius ya silinda; kwa kuzingatia symmetry ya tatizo, uchambuzi unatumia modeli ya robo ya silinda.

Modeli ya uchambuzi wa tatizo la Hertz contact Kielelezo9.1.6 Modeli ya uchambuzi wa tatizo la Hertz contact

(1) Matokeo ya uthibitishaji wa radius ya contact

Fomula ya kinadharia ya kuhesabu radius ya contact ni kama ifuatavyo:

\[ a = \sqrt{\frac{4FR}{\pi E^{*}}} \]

ambapo, [ E^{*} = E/2(1 - \mu^{2}) ] . Chini ya masharti haya ya hesabu, wakati pressure ni \(F=100\), radius ya contact ni \(a=1.36\).

Kielelezo 9.1.7 kinaonyesha equivalent nodal forces katika pointi za contact. Radius ya contact hupatikana kwa kufanya extrapolation ya usambazaji huu wa nguvu za nodi.

Usambazaji wa nguvu sawa za nodi kwenye pointi za contact

Kielelezo9.1.7 Usambazaji wa nguvu sawa za nodi kwenye pointi za contact

(2) Matokeo ya uthibitishaji wa maximum shear stress

Katika suluhisho la kinadharia, katika eneo la contact [ z = 0.78a ] maximum shear stress ni [ \tau_{\max} = 0.30\sqrt{\frac{\text{FE}^{*}}{\pi R}} ] . Chini ya masharti haya ya hesabu, [ \tau_{\max} = 14.2 ] . Kwa kulinganisha, hesabu inatoa [ \tau_{\max} = 15.6 ] .

Usambazaji wa shear stress (thamani ya juu=15.6 Kielelezo9.1.8 Usambazaji wa shear stress (thamani ya juu=15.6)

(3) Uchambuzi wa eigenvalue

Modeli za uthibitishaji za kesi exJ na exK ni sawa na modeli za kesi exA hadi exG. Kielelezo 9.1.9 kinaonyesha mchoro wa dhana wa modeli ya uthibitishaji. Uchambuzi wa eigenvalue unafanywa kwa modeli hii. Eigenvalues za mode ya kwanza hadi ya tatu huhesabiwa. Kesi exJ hutumia iterative solver, wakati exK hutumia direct solver. Matokeo ya uthibitishaji yanaonyeshwa katika Jedwali 9.1.9 hadi Jedwali 9.1.12.

Modeli ya uthibitishaji Kielelezo 9.1.9 Modeli ya uthibitishaji

Natural frequencies za cantilever beam hupatikana kwa milinganyo ifuatayo.

Mode ya kwanza [ n_1 = \frac{1.875^2}{2 \pi l^2} \sqrt{ \frac{gEI}{\omega} } ] Mode ya pili [ n_2 = \frac{4.694^2}{2 \pi l^2} \sqrt{ \frac{gEI}{\omega} } ] Mode ya tatu [ n_3 = \frac{7.855^2}{2 \pi l^2} \sqrt{ \frac{gEI}{\omega} } ]

Thamani za sifa za modeli ya uthibitishaji ni

Kipengee Thamani
\(I\) \(10.0 mm\)
\(E\) \(4000.0 kgf /mm^2\)
\(l\) \(1.0/12.0 mm^4\)
\(\omega\) \(7.85 * 10^{-6} kgf/mm^3\)
\(g\) \(9800.0 mm/sec^2\)

Kwa hiyo, eigenvalues hadi mode ya tatu ni kama ifuatavyo.

Nambari ya mode Thamani
\(n_1\) 3.609e3
\(n_2\) 2.262e4
\(n_3\) 6.335e4
Jedwali 9.1.9 exJ: Matokeo ya uthibitishaji kwa iterative method (eigenvalue ya kwanza)
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: n1=3.609e3 Maelezo
NASTRAN FrontISTR
J231 40 5.861e3 5.861e3 33nodi / tatizo la plane stress
J232 40 3.596e3 3.593e3 105nodi / tatizo la plane stress
J241 20 3.586e3 4.245e3 33nodi / tatizo la plane stress
J242 20 3.590e3 3.587e3 85nodi / tatizo la plane stress
J341 240 5.442e3 5.429e3 99nodi
J342 240 3.621e3 3.595e3 525nodi
J351 80 3.695e3 4.298e3 99nodi
J352 80 3.610e3 3.609e3 381nodi
J361 40 3.679e3 3.619e3 99nodi
J362 40 3.611e3 3.606e3 220nodi
Jedwali 9.1.10 exJ: Matokeo ya uthibitishaji kwa iterative method (eigenvalue ya pili)
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: n2=2.262e4 Maelezo
NASTRAN FrontISTR
J231 40 3.350e4 3.351e4 33nodi / tatizo la plane stress
J232 40 2.163e4 2.156e4 105nodi / tatizo la plane stress
J241 20 2.149e4 2.516e4 33nodi / tatizo la plane stress
J242 20 2.149e4 2.143e4 85nodi / tatizo la plane stress
J341 240 3.145e4 3.138e4 99nodi
J342 240 2.171e4 2.155e4 525nodi
J351 80 2.208e4 2.546e4 99nodi
J352 80 2.156e4 2.149e4 381nodi
J361 40 2.202e4 2.168e4 99nodi
J362 40 2.154e4 2.144e4 220nodi

Kumbuka: Katika modeli za 3D, thamani za mode ya kwanza na ya pili ni mizizi inayolingana. Kwa hiyo, thamani ya mode ya pili katika jedwali inaonyesha thamani ya hesabu ya mode ya tatu.

Jedwali 9.1.11 exK: Matokeo ya uthibitishaji kwa direct method (eigenvalue ya kwanza)
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: n1=3.609e3 Maelezo
NASTRAN FrontISTR
J231 40 5.861e3 5.861e3 33nodi / tatizo la plane stress
J232 40 3.596e3 3.593e3 105nodi / tatizo la plane stress
J241 20 3.586e3 4.245e3 33nodi / tatizo la plane stress
J242 20 3.590e3 3.587e3 85nodi / tatizo la plane stress
J341 240 5.442e3 5.429e3 99nodi
J342 240 3.621e3 3.595e3 525nodi
J351 80 3.695e3 4.298e3 99nodi
J352 80 3.610e3 3.609e3 381nodi
J361 40 3.679e3 3.619e3 99nodi
J362 40 3.611e3 3.606e3 220nodi
J731 40 - 3.606e3 220nodi
J741 20 - 3.594e3 220nodi
Jedwali 9.1.12 exK: Matokeo ya uthibitishaji kwa direct method (eigenvalue ya pili)
Jina la kesi Idadi ya elementi Thamani iliyotabiriwa: n2=2.262e4 Maelezo
NASTRAN FrontISTR
J231 40 3.350e4 3.351e4 33nodi / tatizo la plane stress
J232 40 2.163e4 2.156e4 105nodi / tatizo la plane stress
J241 20 2.149e4 2.516e4 33nodi / tatizo la plane stress
J242 20 2.149e4 2.143e4 85nodi / tatizo la plane stress
J341 240 3.145e4 3.138e4 99nodi
J342 240 2.171e4 2.155e4 525nodi
J351 80 2.208e4 2.546e4 99nodi
J352 80 2.156e4 2.149e4 381nodi
J361 40 2.202e4 2.168e4 99nodi
J362 40 2.154e4 2.144e4 220nodi
J731 40 - 2.156e4 220nodi
J741 20 - 2.153e4 220nodi

Kumbuka: Katika modeli za 3D, thamani za mode ya kwanza na ya pili ni mizizi inayolingana. Kwa hiyo, thamani ya mode ya pili katika jedwali inaonyesha thamani ya hesabu ya mode ya tatu.

(4) Uchambuzi wa upitishaji joto

Masharti ya pamoja ya uchambuzi wa steady-state heat conduction yanaonyeshwa katika Kielelezo 9.1.10. Masharti mahususi ya kesi za uthibitishaji exM hadi exT yanaonyeshwa katika Kielelezo 9.1.11. Mgawanyo wa mesh ni sawa na ule unaotumiwa kwa exA.

Jedwali 9.1.13 hadi Jedwali 9.1.20 yanaonyesha matokeo ya uthibitishaji ya kila kesi kama jedwali la usambazaji wa halijoto.

Uchambuzi wa upitishaji joto

Urefu kati ya A na B \(L = 10.0m\)
Eneo la sehemu ya msalaba \(A = 1.0 mm^2\)

Utegemezi wa thermal conductivity kwa halijoto

Thermal conductivity \(\lambda(W/mK)\) Halijoto \((^\circ C)\)
50.0 0.0
35.0 500.0
20.0 1000.0
Kielelezo 9.1.10 Masharti ya uthibitishaji wa uchambuzi wa steady-state heat conduction
exM:Nyenzo ya mstari
exN:Tatizo la halijoto iliyowekwa
exO:Tatizo la concentrated heat flux
exP:Tatizo la distributed heat flux
exQ:Tatizo la convective heat transfer
exR:Tatizo la radiant heat transfer
exS:Tatizo la volume heat generation
exT:Tatizo la internal gap
Kielelezo 9.1.11 Masharti ya uchambuzi kwa kila kesi ya uthibitishaji
Jedwali 9.1.13 exM: Matokeo ya uthibitishaji wa hesabu ya steady state kwa nyenzo ya mstari
Jina la kesi Aina ya elementi Elementi/nodi Umbali kutoka mwisho A(m)
Mwisho A 2.0 4.0 6.0 8,0 Mwisho B
M361A 361 40/33 0.0 100.0 200.0 300.0 400.0 500.0
M361B 361 40/105 0.0 100.0 200.0 300.0 400.0 500.0
M361C 361 20/33 0.0 100.0 200.0 300.0 400.0 500.0
M361D 361 20/85 0.0 100.0 200.0 300.0 400.0 500.0
M361E 361 240/99 0.0 100.0 200.0 300.0 400.0 500.0
M361F 361 24/525 0.0 100.0 200.0 300.0 400.0 500.0
M361G 361 80/99 0.0 100.0 200.0 300.0 400.0 500.0
Jedwali 9.1.14 exN: Matokeo ya uthibitishaji wa tatizo la halijoto iliyowekwa
Jina la kesi Aina ya elementi Elementi/nodi Umbali kutoka mwisho A(m)
Mwisho A 2.0 4.0 6.0 8,0 Mwisho B
programu ya kibiashara 361 40/99 0.0 87.3 179.7 278.2 384.3 500.0
N231 231 40/33 0.0 87.2 179.5 278.0 384.1 500.0
N232 232 40/105 0.0 86.0 178.3 276.8 382.9 500.0
N241 241 20/33 0.0 87.3 179.7 278.2 384.3 500.0
N242 242 20/85 0.0 87.3 179.7 278.2 384.3 500.0
N341 341 240/99 0.0 87.3 179.7 278.2 384.3 500.0
N342 342 24/525 0.0 87.9 179.9 278.0 383.6 500.0
N351 351 80/99 0.0 87.3 179.7 278.2 384.3 500.0
N352 352 80/381 0.0 87.3 179.7 278.2 384.3 500.0
N361 361 40/99 0.0 87.3 179.7 278.2 384.3 500.0
N362 362 40/330 0.0 87.3 179.7 278.2 384.3 500.0
N731 731 40/33 0.0 87.3 179.7 278.2 384.3 500.0
N741 741 20/33 0.0 87.3 179.7 278.2 384.3 500.0
Jedwali 9.1.15 exO: Matokeo ya uthibitishaji wa tatizo la concentrated heat flux
Jina la kesi Aina ya elementi Elementi/nodi Umbali kutoka mwisho A(m)
Mwisho A 2.0 4.0 6.0 8,0 Mwisho B
programu ya kibiashara 361 40/99 0.0 103.2 213.7 333.3 464.8 612.6
O231 231 40/33 0.0 103.2 213.7 333.3 464.8 612.6
O232 232 40/105 0.0 103.2 213.7 333.3 464.8 612.6
O241 241 20/33 0.0 103.2 213.7 333.3 464.8 612.6
O242 242 20/85 0.0 103.2 213.7 333.4 465.2 618.0
O341 341 240/99 - - - - - -
O342 342 24/525 0.0 104.4 214.9 334.7 466.3 614.6
O351 351 80/99 - - - - - -
O352 352 80/381 0.0 103.2 213.7 333.3 465.0 624.2
O361 361 40/99 0.0 103.2 213.7 333.3 464.8 612.6
O362 362 40/330 0.0 103.2 213.7 333.4 465.5 623.5
O731 731 40/33 0.0 103.2 213.7 333.3 464.8 612.5
O741 741 20/33 0.0 103.2 213.7 333.3 464.8 612.6
Jedwali 9.1.16 exP: Matokeo ya uthibitishaji wa tatizo la distributed heat flux
Jina la kesi Aina ya elementi Elementi/nodi Umbali kutoka mwisho A(m)
Mwisho A 2.0 4.0 6.0 8,0 Mwisho B
programu ya kibiashara 361 40/99 0.0 103.2 213.7 333.3 464.8 612.6
P231 231 40/33 0.0 103.2 213.7 333.3 464.8 612.6
P232 232 40/105 0.0 103.2 213.7 333.3 464.8 612.6
P241 241 20/33 0.0 103.2 213.7 333.3 464.8 612.6
P242 242 20/85 0.0 103.2 213.7 333.3 464.8 612.6
P341 341 240/99 - - - - - -
P342 342 24/525 0.0 103.2 213.7 333.3 464.8 612.6
P351 351 80/99 - - - - - -
P352 352 80/381 0.0 103.2 213.7 333.3 464.8 612.6
P361 361 40/99 0.0 103.2 213.7 333.3 464.8 612.6
P362 362 40/330 0.0 103.2 213.7 333.4 465.5 612.6
P731 731 40/33 0.0 103.2 213.7 333.3 464.8 612.5
P741 741 20/33 0.0 103.2 213.7 333.3 464.8 612.6
Jedwali 9.1.17 exQ: Matokeo ya uthibitishaji wa tatizo la convective heat transfer
Jina la kesi Aina ya elementi Elementi/nodi Umbali kutoka mwisho A(m)
Mwisho A 2.0 4.0 6.0 8,0 Mwisho B
programu ya kibiashara 361 40/99 0.0 89.2 183.8 284.8 393.9 513.2
Q231 231 40/33 0.0 89.2 183.8 284.8 393.9 513.2
Q232 232 40/105 0.0 89.2 183.8 284.8 393.9 513.2
Q241 241 20/33 0.0 89.2 183.8 284.8 393.9 513.2
Q242 242 20/85 0.0 89.2 183.8 284.8 393.9 513.2
Q341 341 240/99 - - - - - -
Q342 342 24/525 0.0 89.2 183.8 284.8 393.9 513.2
Q351 351 80/99 - - - - - -
Q352 352 80/381 0.0 89.2 183.8 284.8 393.9 513.2
Q361 361 40/99 0.0 89.2 183.8 284.8 393.9 513.2
Q362 362 40/330 0.0 89.2 183.8 284.8 393.9 513.2
Q731 731 40/33 0.0 89.2 183.8 284.8 393.9 513.2
Q741 741 20/33 0.0 89.2 183.8 284.8 393.9 513.2
Jedwali 9.1.18 exR: Matokeo ya uthibitishaji wa tatizo la radiant heat transfer
Jina la kesi Aina ya elementi Elementi/nodi Umbali kutoka mwisho A(m)
Mwisho A 2.0 4.0 6.0 8,0 Mwisho B
programu ya kibiashara 361 40/99 0.0 89.5 184.4 285.8 395.3 515.2
R231 231 40/33 0.0 89.5 184.4 285.8 395.3 515.2
R232 232 40/105 0.0 89.5 184.4 285.8 395.3 515.2
R241 241 20/33 0.0 89.5 184.4 285.8 395.3 515.2
R242 242 20/85 0.0 89.5 184.4 285.8 395.3 515.2
R341 341 240/99 - - - - - -
R342 342 24/525 0.0 89.5 184.4 285.8 395.3 515.2
R351 351 80/99 - - - - - -
R352 352 80/381 0.0 89.5 184.4 285.8 395.3 515.2
R361 361 40/99 0.0 89.5 184.4 285.8 395.3 515.2
R362 362 40/330 0.0 89.5 184.4 285.8 395.3 515.2
R731 731 40/33 0.0 89.5 184.4 285.8 395.3 515.2
R741 741 20/33 0.0 89.5 184.4 285.8 395.3 515.2
Jedwali 9.1.19 exS: Matokeo ya uthibitishaji wa tatizo la volume heat generation
Jina la kesi Aina ya elementi Elementi/nodi Umbali kutoka mwisho A(m)
Mwisho A 2.0 4.0 6.0 8,0 Mwisho B
programu ya kibiashara 361 40/99 0.0 103.2 213.7 333.3 464.8 612.6
S231 231 40/33 0.0 103.2 213.7 333.3 464.8 612.6
S232 232 40/105 0.0 103.2 213.7 333.3 464.8 612.6
S241 241 20/33 0.0 103.2 213.7 333.3 464.8 612.6
S242 242 20/85 0.0 103.2 213.7 333.3 464.8 612.6
S341 341 240/99 - - - - - -
S342 342 24/525 0.0 103.2 213.7 333.3 464.8 612.6
S351 351 80/99 - - - - - -
S352 352 80/381 0.0 103.2 213.7 333.3 464.8 612.6
S361 361 40/99 0.0 103.2 213.7 333.3 464.8 612.6
S362 362 40/330 0.0 103.2 213.7 333.3 464.8 612.6
S731 731 40/33 0.0 103.2 213.7 333.3 464.8 612.6
S741 741 20/33 0.0 103.2 213.7 333.3 464.8 612.6
Jedwali 9.1.20 exT: Matokeo ya uthibitishaji wa tatizo la internal gap
Jina la kesi Aina ya elementi Elementi/nodi Umbali kutoka mwisho A(m)
Mwisho A 2.0 4.0 6.0 8,0 Mwisho B
programu ya kibiashara 361 40/99 0.0 88.6 182.4 282.6 387.7 500.0
S231 231 40/33 0.0 88.6 182.4 282.6 387.7 500.0
S232 232 40/105 0.0 88.6 182.4 282.6 387.7 500.0
S241 241 20/33 0.0 88.6 182.4 282.6 387.7 500.0
S242 242 20/85 0.0 88.6 182.4 282.6 387.7 500.0
S341 341 240/99 - - - - - -
S342 342 24/525 0.0 88.6 182.4 282.6 387.7 500.0
S351 351 80/99 - - - - - -
S352 352 80/381 0.0 88.6 182.4 282.6 387.7 500.0
S361 361 40/99 0.0 88.6 182.4 282.6 387.7 500.0
S362 362 40/330 0.0 88.6 182.4 282.6 387.7 500.0
S731 731 40/33 0.0 88.6 182.4 282.6 387.7 500.0
S741 741 20/33 0.0 88.6 182.4 282.6 387.7 500.0

Uchambuzi wa dinamiki wa mstari

Katika exW, uchambuzi wa dinamiki wa mstari unafanywa kwa cantilever beam ileile kama katika kipengee (1). Kielelezo 9.1.12 kinaonyesha masharti ya uthibitishaji. Kwa mgawanyo uleule wa mesh, athari ya nyongeza ya wakati kwenye matokeo inathibitishwa. Mbinu fiche na mbinu wazi za ujumuishaji wa wakati zinatumika, kwa kutumia aina za elementi 361 na 342. Matokeo ya uthibitishaji yanaonyeshwa katika Jedwali 9.1.22 na Kielelezo 9.1.13 hadi Kielelezo 9.1.15.

Modeli ya uchambuzi

Modeli ya uchambuzi

Historia ya wakati ya nguvu ya nje F

Historia ya wakati ya nguvu ya nje F

Suluhisho la kinadharia la uhamisho wa pointi ya msisimko:

\[ F(t)=F_0 I(t) \]

ambapo,

\[ F_0:Constant\ vector \]
\[ I(t)= \begin{cases} 0, t < 0 \\\ 1, 0 \leq t \end{cases} \]
\[ u(t) = \frac{F_0 l^3}{EI} \sum^{\infty}_{i=1} \frac{1-\cos{\omega_i t}}{{\lambda_i}^4} \left\lbrace \cosh{\lambda_i}-\cos{\lambda_i}-\frac{\cosh{\lambda_i} + \cos{\lambda_i}}{\sin{\lambda_i}+\sin{\lambda_i}} (\sinh{\lambda_i} - \sin{\lambda_i}) \right\rbrace^2 \]
Kielelezo 9.1.12 Masharti ya uthibitishaji wa uchambuzi wa dinamiki wa mstari

Masharti ya uthibitishaji:

Urefu \(L\) \(10.0\ mm\)
Upana wa sehemu ya msalaba \(a\) \(1.0\ mm\)
Urefu wa sehemu ya msalaba \(b\) \(1.0\ mm\)
Moduli ya Young \(E\) \(4000.0\ kgf/mm^2\)
Uwiano wa Poisson \(\nu\) \(0.3\)
Msongamano \(\rho\) \(1.0E-09\ kgf\,s^2/mm^3\)
Uharakishaji wa mvuto \(g\) \(9800.0\ mm/s^2\)
Nguvu ya nje \(F_0\) \(1.0\ kgf\)
Elementi Elementi ya hexahedral ya mstari
4 -hedral second-order element
Mbinu ya kutatua mbinu fiche
Kigezo cha mbinu ya Newmark-\(\beta\)\(\gamma\) 1/2
Kigezo cha mbinu ya Newmark-\(\beta\)\(\beta\) 1/4
mbinu wazi
Damping Hakuna
Jedwali 9.1.21 Masharti ya uthibitishaji wa uchambuzi wa dinamiki wa mstari (inaendelea)
Jina la kesi Aina ya elementi Idadi ya nodi Idadi ya elementi Mbinu ya kutatua Nyongeza ya wakati \(\Delta t\) [sec]
W361_c0_im_m2_t1 361 99 40 mbinu fiche 1.0E-06
W361_c0_im_m2_t2 361 99 40 mbinu fiche 1.0E-05
W361_c0_im_m2_t3 361 99 40 mbinu fiche 1.0E-04
W361_c0_ex_m2_t1 361 99 40 mbinu fiche 1.0E-08
W361_c0_ex_m2_t2 361 99 40 mbinu fiche 1.0E-07
W361_c0_ex_m2_t3 361 99 40 mbinu fiche 1.0E-06
W342_c0_im_m2_t1 342 525 240 mbinu wazi 1.0E-06
W342_c0_im_m2_t2 342 525 240 mbinu wazi 1.0E-05
W342_c0_im_m2_t3 342 525 240 mbinu wazi 1.0E-04
W342_c0_ex_m2_t1 342 525 240 mbinu wazi 1.0E-08
W342_c0_ex_m2_t2 342 525 240 mbinu wazi 5.0E-08
W342_c0_ex_m2_t3 342 525 240 mbinu wazi 1.0E-07
Jedwali 9.1.22 exW: Matokeo ya uthibitishaji wa uchambuzi wa dinamiki wa mstari wa cantilever beam
Jina la kesi Aina ya elementi Idadi ya nodi Idadi ya elementi Mbinu Uhamisho wa mwelekeo z katika wakati t=0.002 sec [mm]
W361_c0_im_m2_t1 361 99 40 mbinu fiche 1.9753 1.9302
W361_c0_im_m2_t2 361 99 40 mbinu fiche 1.9753 1.8686
W361_c0_im_m2_t3 361 99 40 mbinu fiche 1.9753 0.3794
W361_c0_ex_m2_t1 361 99 40 mbinu fiche 1.9753 1.9302
W361_c0_ex_m2_t2 361 99 40 mbinu fiche 1.9753 1.9247
W361_c0_ex_m2_t3 361 99 40 mbinu fiche 1.9753 Diverged
W342_c0_im_m2_t1 342 525 240 mbinu wazi 1.9753 1.9431
W342_c0_im_m2_t2 342 525 240 mbinu wazi 1.9753 1.8719
W342_c0_im_m2_t3 342 525 240 mbinu wazi 1.9753 0.3873
W342_c0_ex_m2_t1 342 525 240 mbinu wazi 1.9753 1.9359
W342_c0_ex_m2_t2 342 525 240 mbinu wazi 1.9753 1.9358
W342_c0_ex_m2_t3 342 525 240 mbinu wazi 1.9753 Diverged

Mchoro wa deformation na usambazaji wa mkazo sawa wa cantilever

Kielelezo 9.1.13 Mchoro wa deformation na usambazaji wa mkazo sawa wa cantilever

(a) Aina ya elementi 361:mbinu fiche

(a) Aina ya elementi 361:mbinu fiche

(b) Aina ya elementi 361:mbinu wazi

(b) Aina ya elementi 361:mbinu wazi
Kielelezo 9.1.14 Historia ya wakati ya uhamisho wa pointi ya msisimko \(u_z\)

(a) Aina ya elementi 342:mbinu fiche

(a) Aina ya elementi 342:mbinu fiche

(b) Aina ya elementi 342:mbinu wazi

(b) Aina ya elementi 342:mbinu wazi
Kielelezo 9.1.14 Historia ya wakati ya uhamisho wa pointi ya msisimko \(u_z\)

Uchambuzi wa frequency response

Katika uthibitishaji huu, uchambuzi wa frequency response unafanywa kwa cantilever beam na kuthibitishwa kwa kulinganisha na matokeo ya general-purpose commercial solver. Modeli ya uchambuzi na masharti ya uthibitishaji yanaonyeshwa hapa chini.

Masharti ya uchambuzi:

Moduli ya Young \(E\) \(210000\ N/mm^2\)
Uwiano wa Poisson \(\nu\) \(0.3\)
Msongamano \(\rho\) \(7.89E-09\ t/mm^3\)
Uharakishaji wa mvuto \(g\) \(9800.0\ mm/s^2\)
Mzigo \(F_0\) \(1.0\ N\)
Kigezo cha Rayleigh damping \(R_m\) \(0.0\)
Kigezo cha Rayleigh damping \(R_k\) \(7.2E-07\)
Kielelezo 9.1.15 Modeli ya uchambuzi(tetrahedrallinear element(Idadi ya elementi126、Idadi ya nodi55))

Eigenvalues hadi mode ya tano na frequency response ya pointi za msisimko zilizopatikana kutoka uchambuzi wa eigenvalue zinaonyeshwa kama ifuatavyo.

Mode FrontISTR programu ya kibiashara
1 14952 14952
2 15002 15003
3 84604 84539
4 84771 84697
5 127054 126852

Utegemezi wa frequency wa ukubwa wa uhamisho wa pointi ya msisimko

Kielelezo 9.1.16 Utegemezi wa frequency wa ukubwa wa uhamisho wa pointi ya msisimko
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