The document analyzes the forces, moments, and reactions in a beam-column structure. It calculates the internal forces including shear forces and bending moments at various points along the beams. Diagrams are drawn showing the shear force and bending moment diagrams. The maximum bending moment of 51.68 tm occurs at a point 3.46 m from end C of the beam.
Influence of MHD on Unsteady Helical Flows of Generalized Oldoyd-B Fluid betw...IJERA Editor
Considering a fractional derivative model for unsteady magetohydrodynamic (MHD)helical flows of an
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(MHD)helical flows of an Oldoyd-B fluid in an annular pipe are obtained under series form in terms of
Mittag –leffler function,satisfy all imposed initial and boundary condition , Finally the influence of model
parameters on the velocity and shear stress are analyzed by graphical illustrations.
Influence of MHD on Unsteady Helical Flows of Generalized Oldoyd-B Fluid betw...IJERA Editor
Considering a fractional derivative model for unsteady magetohydrodynamic (MHD)helical flows of an
Oldoyd-B fluid in concentric cylinders and circular cylinder are studied by using finite Hankel and Laplace
transforms .The solution of velocity fields and the shear stresses of unsteady magetohydrodynamic
(MHD)helical flows of an Oldoyd-B fluid in an annular pipe are obtained under series form in terms of
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Salah satu materi perkuliahan prodi pendidikan matematika mata kuliah teori himpunan dan logika matematika - Diagram Venn, Contoh Soal mengenai Diagram Venn
Diseno en ingenieria mecanica de Shigley - 8th ---HDes
descarga el contenido completo de aqui http://paralafakyoumecanismos.blogspot.com.ar/2014/08/libro-para-mecanismos-y-elementos-de.html
Influence line for determinate structure(with detailed calculation)Md. Ragib Nur Alam
Influence Line of determinate beams and frames( Various types) are drawn using Brute force method with detailed calculation. Professor Dr. Tarif Uddin Ahmed, Dept. of CE, RUET asked us to solve 23 different sets of problems. I made a solution of these problems using Autocad by myself with all details that can be possibly shown. - Md. Ragib Nur Alam, CE -13, RUET. Copyright reserved.
Diseno en ingenieria mecanica de Shigley - 8th ---HDes
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Macroeconomics- Movie Location
This will be used as part of your Personal Professional Portfolio once graded.
Objective:
Prepare a presentation or a paper using research, basic comparative analysis, data organization and application of economic information. You will make an informed assessment of an economic climate outside of the United States to accomplish an entertainment industry objective.
Model Attribute Check Company Auto PropertyCeline George
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Diseno en ingenieria mecanica de Shigley - 8th ---HDes
descarga el contenido completo de aqui http://paralafakyoumecanismos.blogspot.com.ar/2014/08/libro-para-mecanismos-y-elementos-de.html
Influence line for determinate structure(with detailed calculation)Md. Ragib Nur Alam
Influence Line of determinate beams and frames( Various types) are drawn using Brute force method with detailed calculation. Professor Dr. Tarif Uddin Ahmed, Dept. of CE, RUET asked us to solve 23 different sets of problems. I made a solution of these problems using Autocad by myself with all details that can be possibly shown. - Md. Ragib Nur Alam, CE -13, RUET. Copyright reserved.
Diseno en ingenieria mecanica de Shigley - 8th ---HDes
descarga el contenido completo de aqui http://paralafakyoumecanismos.blogspot.com.ar/2014/08/libro-para-mecanismos-y-elementos-de.html
Macroeconomics- Movie Location
This will be used as part of your Personal Professional Portfolio once graded.
Objective:
Prepare a presentation or a paper using research, basic comparative analysis, data organization and application of economic information. You will make an informed assessment of an economic climate outside of the United States to accomplish an entertainment industry objective.
Model Attribute Check Company Auto PropertyCeline George
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1. NAMA : ANDRE CHANDRA ANALISIS STRUKTUR - MEKANIKA TEKNIK
NIM : 1422201013 DOSEN : IR. VIRGO TRISEP HARIS M.T
BALOK GERBER
S1
S2
S1
RVS2
RVS1
M = 10 tm
P = 7 t
C
MC
Q = 10 t/m’
RVC
BA
P = 6 t
RVA RVB
S2
M = 10 tm
Q = 10 t/m’
P = 7 t
P = 6 t
C
6 44222 2 2 22
BA
2. NAMA : ANDRE CHANDRA ANALISIS STRUKTUR - MEKANIKA TEKNIK
NIM : 1422201013 DOSEN : IR. VIRGO TRISEP HARIS M.T
MENGHITUNG REAKSI PERLETAKAN
𝑀𝑆2 = 0
RVS1 (6) – P (4) + M = 0
RVS1 (6) – 7 (4) + 10 = 0
RVS1 (6) – 18 = 0
RVS1 (6) = 18
RVS1 = 3 t
2 4
S2
S1
RVS2
RVS1
M = 10 t/m’
P = 7 t
𝑀𝑆1 = 0
-RVS2 (6) + P (2) + M = 0
-RVS2 (6) + 7 (2) + 10 = 0
-RVS2 (6) + 24 = 0
RVS2 (6) = 24
RVS2 = 4 t
𝐾𝑜𝑛𝑡𝑟𝑜𝑙 ∶ V = 0
RVS1 + RVS2 – P = 0
3 + 4 – 7 = 0
44
P’
𝑀 = 0
MC – P’ (6) – RVS2 (8) = 0
MC – 40 (6) – 4 (8) = 0
MC – 272 = 0
MC = 272 tm
𝑉 = 0
RVC – RVS2 – P’ = 0
RVC – 4 – 40 = 0
RVC – 44 = 0
RVC = 44 t
22
RVS2 = 4 t
C
MC
Q = 10 t/m’
RVC
P’ = q . l
P’ = 10 (4)
P’ = 40 t
3. NAMA : ANDRE CHANDRA ANALISIS STRUKTUR - MEKANIKA TEKNIK
NIM : 1422201013 DOSEN : IR. VIRGO TRISEP HARIS M.T
𝑀𝐵 = 0
RVA (10) – P’ (4) +P (2) + RVS1 (2) = 0
RVA (10) – 36 (4) + 6 (2) + 3 (2) = 0
RVA (10) – 120 = 0
RVA (10) =120
RVA = 12 t
𝑀𝐴 = 0
RVS1 (14) + P (12) – RVB (10) + P’ (6) = 0
3 (14) + 6 (12) – RVB (10) + 36 (6) = 0
330 – RVB (10) = 0
RVB (10) = 330
RVB = 33 t
P’ = ½ q.l
P’ = ½ 12 (6)
P’ = 36 t
𝐾𝑜𝑛𝑡𝑟𝑜𝑙 ∶ 𝑉 = 0
RVA + RVB – P’ – P – RVS1 = 0
12 + 33 – 36 – 6 – 3 = 0
24
P’
BA
RVS1 = 3 t
P = 6 t
RVA RVB
2 6 22 2
4. NAMA : ANDRE CHANDRA ANALISIS STRUKTUR - MEKANIKA TEKNIK
NIM : 1422201013 DOSEN : IR. VIRGO TRISEP HARIS M.T
MENGGAMBAR DIAGRAM GAYA LINTANG, GAYA NORMAL, & MOMEN
R
X1 (0° ≤ α𝑥1 ≤ 48,18°) (S1 – R)
NX1 = - RVS1 cos α𝑥1 = - 3 cos α𝑥1
α𝑥1 = 0° NS1 = - 3 cos 0°
NS1 = - 3 t
α𝑥1 = 48,18° NR = - 3 cos 48,18°
NR = - 2 t
X2 (0° ≤ α𝑥2 ≤ 41,81°) (S2 – R)
NX2 = RVS2 sin α𝑥2 = 4 sin α𝑥2
α𝑥2 = 0° NS2 = 4 sin 0°
NS2 = 0 t
α𝑥2 = 41,81° NR = 4 sin 41,81°
NR = 2,66 t
PNPQ
X2
X1
R
α
cos α =
4
6
= 0,66 sin α = 0,74
α = 48,18° 90°- α = 41,81°
α
X1 (0° ≤ α𝑥1 ≤ 48,18°) (S1 – R)
QX1 = RVS1 sin α𝑥1 = 3 sin α𝑥1
α𝑥1 = 0° QS1 = 3 sin 0°
QS1 = 0 t
α𝑥1 = 48,18° QR = 3 sin 48,18°
QR = 2,23 t
2 4
M = 10 t/m’
RVS2 = 4 t
S2
S1
RVS1 = 3 t
P = 7 t
X2 (0° ≤ α𝑥2 ≤ 41,81°) (S2 – R)
QX2 = - RVS2 cos α𝑥2 = - 4 cos α𝑥2
α𝑥2 = 0° QS2 = - 4 cos 0°
QS2 = - 4 t
α𝑥2 = 41,81° QR = - 4 cos 41,81°
QR = -2,98 t
R S2
2,23
S1
-2,98
-4
-3
-2
S1 S2
2,66
R
GAYA NORMAL (N)
GAYA LINTANG (Q)
6. NAMA : ANDRE CHANDRA ANALISIS STRUKTUR - MEKANIKA TEKNIK
NIM : 1422201013 DOSEN : IR. VIRGO TRISEP HARIS M.T
B
BC = 42 + 62
BC = 52
BC = 7,21
α
A
X1
6
44
P’= 40 t
0 ≤ 𝑥1≤4 (A – B)
QX1 = - RVS2 – P’x = - 4 – 10x
𝑥1 = 0 QA = - 4 – 10 (0)
QA = - 4 t
𝑥1 = 4 QB = - 4 – 10 (4)
QB = - 44 t
0 ≤ 𝑥2≤7,21 (C – B)
QX2 = - RVC cos α = - 44
4
7,21
= - 24,41 t
𝑥2 = 0 QC = - 24,41 t
𝑥2 = 7,21 QB = - 24,41 t
22
RVS2 = 4 t
C
MC = 272 tm
Q = 10 t/m’
RVC = 44 t
P’x = q.x
P’x = 10x
P’x
cos α =
4
7,21
sin α =
6
7,21
-24,41
-44
B CA
-4
0 ≤ 𝑥1≤4 (A – B)
NX1 = 0 t
𝑥1 = 0 NA = 0
𝑥1 = 4 NB = 0
(tidak ada gaya yang sejajar sumbu batang)
0 ≤ 𝑥2≤7,21 (C – B)
NX2 = - RVC sin α = - 44
6
7,21
= - 36,52 t
𝑥2 = 0 NC = - 36,52 t
𝑥2 = 7,21 NB = - 36,52 t
-36,52
B CA
GAYA NORMAL (N)
GAYA LINTANG (Q)
7. NAMA : ANDRE CHANDRA ANALISIS STRUKTUR - MEKANIKA TEKNIK
NIM : 1422201013 DOSEN : IR. VIRGO TRISEP HARIS M.T
B
X2
A
X1
44
P’= 40 t
0 ≤ 𝑥1≤4 (A – B)
MX1 = - RVS2 (𝑥1) – P’x (½ 𝑥1) = - 4(𝑥1) – 10x (½ 𝑥1)
𝑥1 = 0 MA = - 4 (0) – 10 (0)(0)
MA = 0 tm
𝑥1 = 4 MB = - 4 (4) – 10 (4)(2)
MB = - 96 tm
0 ≤ 𝑥2≤ 4 (C – B)
MX1 = RVC (𝑥2) – MC = 44(𝑥2) - 272
𝑥2 = 0 MC = 44 (0) – 272
MC = - 272 tm
𝑥2 = 4 MB = 44 (4) – 272
MB = - 96 tm
22
RVS2 = 4 t
C
MC = 272 tm
Q = 10 t/m’
RVC = 44 t
P’x = q.x
P’x = 10x
P’x
CBA
-272
-96
MOMEN (M)
8. NAMA : ANDRE CHANDRA ANALISIS STRUKTUR - MEKANIKA TEKNIK
NIM : 1422201013 DOSEN : IR. VIRGO TRISEP HARIS M.T
X5 X4
X3X2X1
P’x
DC E F
0≤𝑥2≤6 (C – D)
QX2 = RVA – P’x = 12 – 𝑥2
𝑥2 = 0 QC = 12 – 02
QC = 12 t
𝑥2 = 6 QD = 12 – 62
QD = - 24 t
P’ = ½ q.l
P’ = ½ 12 (6)
P’ = 36 t
0≤𝑥3≤2 (D – B)
QX3 = RVA – P’ = 12 –36
= - 24
𝑥3 = 0 QD = - 24 t
𝑥3 = 2 QB = - 24 t24
P’ = 36 t
BA
RVS1 = 3 t
P = 6 t
RVA = 12 t RVB = 33 t
2 6 22 2
0≤𝑥1≤2 (A – C)
QX1 = RVA = 12
𝑥1 = 0 QA = 12 t
𝑥1 = 2 QC = 12 t
P’x = ½ qx(
𝑥
𝑙
)
P’x = ½ 12 x(
𝑥
6
)
P’x = 𝑥2
0≤𝑥4≤2 (F – E)
QX1 = RVS1 = 3
𝑥4 = 0 QF = 3 t
𝑥4 = 2 QE = 3 t
0≤𝑥5≤2 (E – B)
QX2 = RVS1 + P = 3 + 6 = 9
𝑥5 = 0 QE = 9 t
𝑥5 = 2 QB = 9 t
3
9
-24
12
y
𝑥2
= 12
Y = 2 + 𝑥2
QX2 = 0
QX2 = 12 – 𝑥2
12 – 𝑥2
= 0
x = 3,46
GAYA LINTANG (Q)
9. NAMA : ANDRE CHANDRA ANALISIS STRUKTUR - MEKANIKA TEKNIK
NIM : 1422201013 DOSEN : IR. VIRGO TRISEP HARIS M.T
GAYA NORMAL (N) Tidak ada Gaya Normal yang terjadi karena tidak ada
gaya yang sejajar sumbu batang.
MOMEN (M)
0≤𝑥1≤2 (A – C)
MX1 = RVA(𝑥1) = 12(𝑥1)
𝑥1 = 0 MA = 12 (0) = 0 tm
𝑥1 = 2 MC = 12 (2) = 24 tm
0≤𝑥2≤6 (C – D)
MX2 = RVA(2 + 𝑥2) – P’x(
1
3
𝑥2 )
MX2 = 12(2 + 𝑥2) – 𝑥2
(
1
3
𝑥2 )
𝑥2 = 0 MC = 12(2+0) – 02
(
1
3
(0))
MC = 24 tm
𝑥2 = 6 MD = 12(2+6) – 62
(
1
3
(6))
MD = 24 tm
𝑥2 = 3,46 𝑀 𝑚𝑎𝑥 = 12(2+3,46) – 3,462
(
1
3
(3,46))
𝑀 𝑚𝑎𝑥 = 51,68 tm
0≤𝑥4≤2 (F – E)
MX4 = - RVS1(𝑥4) = - 3(𝑥4)
𝑥4 = 0 MF = - 3 (0) = 0 tm
𝑥4 = 2 ME = - 3 (2) = - 6 tm
0≤𝑥3≤6 (D – B)
MX3 = RVA(8 + 𝑥2) – P’(2 + 𝑥2)
MX3 = 12(8 + 𝑥2) – 36 (2 + 𝑥2)
𝑥2 = 0 MD = 12(8+0) – 36 (2+0)
MD = 24 tm
𝑥2 = 6 MB = 12(8+2) – 36 (2+2)
MB = -24 tm 0≤𝑥5≤2 (E – B)
MX3 = - RVS1(2 + 𝑥5) – P(𝑥5)
MX3 = - 3(2 + 𝑥5) – 6(𝑥5)
𝑥2 = 0 ME = -3(2+0) – 6(0)
ME = -6 tm
𝑥2 = 2 MB = 12(2+2) – 36 (2)
MB = -24 tm
-24
-6
FB E
DCA
24
51,68
24