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C H. DER. Nº 1CALCULO DE LOS ELEMENTOS ESPIRAL CURVA ESPIRAL
DATOS DE DISEÑO
V(Diseño)= 25 Km/hRc= 20 mα= 92.2475 ˚PI= 0+024.055 m.A= 20n= 2
ANCH0 VIA= 6 m.
REQUERIMIENTO DE UTILIZACION DE CURVAS DE TRANSICIÓN:
0.098xV^261.25SI NECESITA CURVAS DE TRANSICIÓN
CALCULOS
Le(min)= (0.036xV^3)/RLe(min)= 28.125
A= (Le*R)^0.5Le= (A^2)/R
RMT=
RMT=
RMT>Rc
Le= 20Le>Le(min) CORREGIR A
δe= Le/2Rδe= 0.5θe=θe= 28.64788976θe=θe= 28.64788976Ae= (θe/3)-θex8.3x10^(-7)Ae= 9.549272808
B= θe-AeB= 19.09861695
Xe= Lex(1-((δe^2)/10)+((δe^4)/216)+((δe^6)/9360)+((δe^8)/685440))Xe= 19.50582054Ye= Lex(((δe^2)/3)+((δe^3)/42)+((δe^5)/1320)+((δe^7)/75600))Ye= 3.274280942
u=u= 13.51228948v=v= 6.829592248
P=P= 0.82593218K=K= 9.917309766
CURAVAS SIMETRICAS
Te=Te= 31.57661766αc= α-2θeαc= 34.95172049Lc= πxRx(αc/180)Lc= 12.20045203
Lc+2Le52.20045203
πxRx(α/180)+Le52.20045203
TE= PI-TeTE= -0+007.522EC= TE+LeEC= 0+012.478CE= EC+LeCE= 0+024.679ET= CE+LeET= 0+044.679ET= TE+LTET= 0+044.679
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)
180xδe/π
90xLe/πxR
Xe-(Ye/Tanθe)
Ye/(Senθe)
Ye-r(1-Cosθe)
Xe-R(Senθe)
(R+P)*Tg(α/2)+K
LT=LT=LT=LT=
S= 2.339126885 m/mP= (V^2/(127xR))-fP= 0.166062992 m/mP= 16.60629921 %
C H. IZQ. Nº 2CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 28.538889 ˚PI= 0+085.120 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 62R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 30.8820497103
T= RxTan(α/2)T= 15.7683940565
E= Rx(Sec(α/2)-1)E= 1.97376220859
M= R-RxCos(α/2)
M= 1.91286634875959
Gc=Gc= 18.4825095203
Gc*l/20
21.2548859484
C=C= 22.86834366
CL=CL= 30.5637935851
θ/2
10.6274429742
Gc*l/40
10.6274429742
PC= PI-TPC= 0+069.352PT= PC+LcPT= 0+100.234
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 1.19772911623P= (V^2/(127xR))-fP= 0.192500635 m/mP= 19.2500635001 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. DER. Nº 3CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 16.513333 ˚PI= 0+138.578 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 130R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 37.467564829
T= RxTan(α/2)T= 18.8645473792
E= Rx(Sec(α/2)-1)E= 1.3616045419
M= R-RxCos(α/2)
M= 1.34749108054893
Gc=Gc= 8.8147353097
Gc*l/20
10.1369456062
C=C= 22.9700142005
CL=CL= 37.3380207687
θ/2
5.06847280308
Gc*l/40
5.06847280308
PC= PI-TPC= 0+119.713PT= PC+LcPT= 0+157.181
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 0.70643626792P= (V^2/(127xR))-fP= 0.02642337977 m/mP= 2.64233797698 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. IZQ. Nº 4CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 17.961667 ˚PI= 0+191.855 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 108.415R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 33.9870424701
T= RxTan(α/2)T= 17.13407414
E= Rx(Sec(α/2)-1)E= 1.34559730903
M= R-RxCos(α/2)
M= 1.32910111492497
Gc=Gc= 10.5697144331
Gc*l/20
12.155171598
C=C= 22.9568928622
CL=CL= 33.8480418917
θ/2
6.07758579902
Gc*l/40
6.07758579902
PC= PI-TPC= 0+174.721PT= PC+LcPT= 0+208.708
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 0.80152260742P= (V^2/(127xR))-fP= 0.05657117899 m/mP= 5.65711789889 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. DER. Nº 5CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 31.368333 ˚PI= 0+245.647 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 122.593R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 67.1173011523
T= RxTan(α/2)T= 34.4227865351
E= Rx(Sec(α/2)-1)E= 4.74109551979
M= R-RxCos(α/2)
M= 4.56456788486173
Gc=Gc= 9.34731665154
Gc*l/20
10.7494141493
C=C= 22.9662829293
CL=CL= 66.2822106283
θ/2
5.37470707463
Gc*l/40
5.37470707463
PC= PI-TPC= 0+211.224PT= PC+LcPT= 0+278.342
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 0.73569487309P= (V^2/(127xR))-fP= 0.03557229507 m/mP= 3.55722950746 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. IZQ. Nº 6CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 21.785000 ˚PI= 0+331.590 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 78.429R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 29.820272619
T= RxTan(α/2)T= 15.092398099
E= Rx(Sec(α/2)-1)E= 1.43894426664
M= R-RxCos(α/2)
M= 1.41301946512857
Gc=Gc= 14.6108657545
Gc*l/20
16.8024956177
C=C= 22.9176711539
CL=CL= 29.640970514
θ/2
8.40124780885
Gc*l/40
8.40124780885
PC= PI-TPC= 0+316.498PT= PC+LcPT= 0+346.318
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 1.00905867811P= (V^2/(127xR))-fP= 0.12599184447 m/mP= 12.5991844472 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. DER. Nº 7CALCULO DE LOS ELEMENTOS ESPIRAL CURVA ESPIRAL
DATOS DE DISEÑO
V(Diseño)= 25 Km/hRc= 35 mα= 33.39777778 ˚PI= 0+431.103 m.A= 24n= 2
ANCH0 VIA= 6 m.
REQUERIMIENTO DE UTILIZACION DE CURVAS DE TRANSICIÓN:
0.098xV^261.25SI NECESITA CURVAS DE TRANSICIÓN
CALCULOS
Le(min)= (0.036xV^3)/RLe(min)= 16.07142857
A= (Le*R)^0.5Le= (A^2)/R
RMT=
RMT=
RMT>Rc
Le= 16.45714286Le>Le(min) Ok
δe= Le/2Rδe= 0.235102041θe=θe= 13.47035469θe=θe= 13.47035469Ae= (θe/3)-θex8.3x10^(-7)Ae= 4.490107051
B= θe-AeB= 8.980247643
Xe= Lex(1-((δe^2)/10)+((δe^4)/216)+((δe^6)/9360)+((δe^8)/685440))Xe= 16.36641241Ye= Lex(((δe^2)/3)+((δe^3)/42)+((δe^5)/1320)+((δe^7)/75600))Ye= 1.284619735
u=u= 11.00336322v=v= 5.514756974
P=P= 0.321789922K=K= 8.213434692
CURAVAS SIMETRICAS
Te=Te= 18.80973289αc= α-2θeαc= 6.45706839Lc= πxRx(αc/180)Lc= 3.94439862
Lc+2Le36.85868433
πxRx(α/180)+Le36.85868433
TE= PI-TeTE= 0+412.293EC= TE+LeEC= 0+428.750CE= EC+LeCE= 0+432.695ET= CE+LeET= 0+449.152ET= TE+LTET= 0+449.152
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)
180xδe/π
90xLe/πxR
Xe-(Ye/Tanθe)
Ye/(Senθe)
Ye-r(1-Cosθe)
Xe-R(Senθe)
(R+P)*Tg(α/2)+K
LT=LT=LT=LT=
S= 1.42431628 m/mP= (V^2/(127xR))-fP= 0.060607424 m/mP= 6.060742407 %
C H. IZQ. Nº 8CALCULO DE LOS ELEMENTOS ESPIRAL CURVA ESPIRAL
DATOS DE DISEÑO
V(Diseño)= 25 Km/hRc= 15 mα= 120.7066667 ˚PI= 0+493.971 m.A= 20n= 2
ANCH0 VIA= 6 m.
REQUERIMIENTO DE UTILIZACION DE CURVAS DE TRANSICIÓN:
0.098xV^261.25SI NECESITA CURVAS DE TRANSICIÓN
CALCULOS
Le(min)= (0.036xV^3)/RLe(min)= 37.5
A= (Le*R)^0.5Le= (A^2)/R
RMT=
RMT=
RMT>Rc
Le= 26.66666667Le>Le(min) CORREGIR A
δe= Le/2Rδe= 0.888888889θe=θe= 50.92958179θe=θe= 50.92958179Ae= (θe/3)-θex8.3x10^(-7)Ae= 16.97648499
B= θe-AeB= 33.9530968
Xe= Lex(1-((δe^2)/10)+((δe^4)/216)+((δe^6)/9360)+((δe^8)/685440))Xe= 24.63816474Ye= Lex(((δe^2)/3)+((δe^3)/42)+((δe^5)/1320)+((δe^7)/75600))Ye= 7.466365538
u=u= 18.5768122v=v= 9.616995841
P=P= 1.920491302K=K= 12.99258592
CURAVAS SIMETRICAS
Te=Te= 42.72163144αc= α-2θeαc= 18.84750309Lc= πxRx(αc/180)Lc= 4.93426477
Lc+2Le58.2675981
πxRx(α/180)+Le58.2675981
TE= PI-TeTE= 0+451.249EC= TE+LeEC= 0+477.916CE= EC+LeCE= 0+482.850ET= CE+LeET= 0+509.517ET= TE+LTET= 0+509.517
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)
180xδe/π
90xLe/πxR
Xe-(Ye/Tanθe)
Ye/(Senθe)
Ye-r(1-Cosθe)
Xe-R(Senθe)
(R+P)*Tg(α/2)+K
LT=LT=LT=LT=
S= 3.063619116 m/mP= (V^2/(127xR))-fP= 0.24808399 m/mP= 24.80839895 %
C H. DER. Nº 9CALCULO DE LOS ELEMENTOS ESPIRAL CURVA ESPIRAL
DATOS DE DISEÑO
V(Diseño)= 25 Km/hRc= 55 mα= 65.00416667 ˚PI= 0+624.016 m.A= 25n= 2
ANCH0 VIA= 6 m.
REQUERIMIENTO DE UTILIZACION DE CURVAS DE TRANSICIÓN:
0.098xV^261.25SI NECESITA CURVAS DE TRANSICIÓN
CALCULOS
Le(min)= (0.036xV^3)/RLe(min)= 10.22727273
A= (Le*R)^0.5Le= (A^2)/R
RMT=
RMT=
RMT>Rc
Le= 11.36363636Le>Le(min) Ok
δe= Le/2Rδe= 0.103305785θe=θe= 5.918985487θe=θe= 5.918985487Ae= (θe/3)-θex8.3x10^(-7)Ae= 1.97299025
B= θe-AeB= 3.945995237
Xe= Lex(1-((δe^2)/10)+((δe^4)/216)+((δe^6)/9360)+((δe^8)/685440))Xe= 11.35151499Ye= Lex(((δe^2)/3)+((δe^3)/42)+((δe^5)/1320)+((δe^7)/75600))Ye= 0.391011601
u=u= 7.579996864v=v= 3.791732984
P=P= 0.09779017K=K= 5.679797556
CURAVAS SIMETRICAS
Te=Te= 40.78377769αc= α-2θeαc= 53.16619569Lc= πxRx(αc/180)Lc= 51.03588411
Lc+2Le73.76315684
πxRx(α/180)+Le73.76315684
TE= PI-TeTE= 0+583.232EC= TE+LeEC= 0+594.596CE= EC+LeCE= 0+645.632ET= CE+LeET= 0+656.995ET= TE+LTET= 0+656.995
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)
180xδe/π
90xLe/πxR
Xe-(Ye/Tanθe)
Ye/(Senθe)
Ye-r(1-Cosθe)
Xe-R(Senθe)
(R+P)*Tg(α/2)+K
LT=LT=LT=LT=
S= 0.971840365 m/mP= (V^2/(127xR))-fP= 0.009477452 m/mP= 0.947745168 %
C H. IZQ. Nº 10CALCULO DE LOS ELEMENTOS ESPIRAL CURVA ESPIRAL
DATOS DE DISEÑO
V(Diseño)= 25 Km/hRc= 25 mα= 81.04861111 ˚PI= 0+696.391 m.A= 25n= 2
ANCH0 VIA= 6 m.
REQUERIMIENTO DE UTILIZACION DE CURVAS DE TRANSICIÓN:
0.098xV^261.25SI NECESITA CURVAS DE TRANSICIÓN
CALCULOS
Le(min)= (0.036xV^3)/RLe(min)= 22.5
A= (Le*R)^0.5Le= (A^2)/R
RMT=
RMT=
RMT>Rc
Le= 25Le>Le(min) Ok
δe= Le/2Rδe= 0.5θe=θe= 28.64788976θe=θe= 28.64788976Ae= (θe/3)-θex8.3x10^(-7)Ae= 9.549272808
B= θe-AeB= 19.09861695
Xe= Lex(1-((δe^2)/10)+((δe^4)/216)+((δe^6)/9360)+((δe^8)/685440))Xe= 24.38227567Ye= Lex(((δe^2)/3)+((δe^3)/42)+((δe^5)/1320)+((δe^7)/75600))Ye= 4.092851177
u=u= 16.89036185v=v= 8.53699031
P=P= 1.032415225K=K= 12.39663721
CURAVAS SIMETRICAS
Te=Te= 34.64952598αc= α-2θeαc= 23.7528316Lc= πxRx(αc/180)Lc= 10.36412795
Lc+2Le60.36412795
πxRx(α/180)+Le60.36412795
TE= PI-TeTE= 0+661.741EC= TE+LeEC= 0+686.741CE= EC+LeCE= 0+697.106ET= CE+LeET= 0+722.106ET= TE+LTET= 0+722.106
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)
180xδe/π
90xLe/πxR
Xe-(Ye/Tanθe)
Ye/(Senθe)
Ye-r(1-Cosθe)
Xe-R(Senθe)
(R+P)*Tg(α/2)+K
LT=LT=LT=LT=
S= 1.912347247 m/mP= (V^2/(127xR))-fP= 0.116850394 m/mP= 11.68503937 %
C H. DER. Nº11CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 24.636111 ˚PI= 0+826.856 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 268.965R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 115.649907922
T= RxTan(α/2)T= 58.7326479413
E= Rx(Sec(α/2)-1)E= 6.3379152755
M= R-RxCos(α/2)
M= 6.19200628649355
Gc=Gc= 4.26046359289
Gc*l/20
4.89953313182
C=C= 22.9929928562
CL=CL= 114.761056109
θ/2
2.44976656591
Gc*l/40
2.44976656591
PC= PI-TPC= 0+768.123PT= PC+LcPT= 0+883.773
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 0.43431283147P= (V^2/(127xR))-fP= -0.0518118924 m/mP= -5.1811892365 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. IZQ. Nº12CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 4.145000 ˚PI= 0+979.137 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 691.164R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 50.0014975683
T= RxTan(α/2)T= 25.011658236
E= Rx(Sec(α/2)-1)E= 0.45240953907
M= R-RxCos(α/2)
M= 0.452113602785744
Gc=Gc= 1.65795034212
Gc*l/20
1.90664289344
C=C= 22.9989387834
CL=CL= 49.9905945394
θ/2
0.95332144672
Gc*l/40
0.95332144672
PC= PI-TPC= 0+954.125PT= PC+LcPT= 1+004.127
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 0.2405516269P= (V^2/(127xR))-fP= -0.0965190036 m/mP= -9.6519003637 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. DER. Nº13CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 7.918889 ˚PI= 1+022.970 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 217.057R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 29.9995964827
T= RxTan(α/2)T= 15.0237213612
E= Rx(Sec(α/2)-1)E= 0.51931638701
M= R-RxCos(α/2)
M= 0.518076870157614
Gc=Gc= 5.27933026929
Gc*l/20
6.07122980969
C=C= 22.9892412028
CL=CL= 29.9757247631
θ/2
3.03561490484
Gc*l/40
3.03561490484
PC= PI-TPC= 1+007.946PT= PC+LcPT= 1+037.946
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 0.49977980175P= (V^2/(127xR))-fP= -0.0343093548 m/mP= -3.4309354823 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. DER. Nº 14CALCULO DE LOS ELEMENTOS ESPIRAL CURVA ESPIRAL
DATOS DE DISEÑO
V(Diseño)= 25 Km/hRc= 15 mα= 108.1933333 ˚PI= 1+082.342 m.A= 15n= 2
ANCH0 VIA= 6 m.
REQUERIMIENTO DE UTILIZACION DE CURVAS DE TRANSICIÓN:
0.098xV^261.25SI NECESITA CURVAS DE TRANSICIÓN
CALCULOS
Le(min)= (0.036xV^3)/RLe(min)= 37.5
A= (Le*R)^0.5Le= (A^2)/R
RMT=
RMT=
RMT>Rc
Le= 15Le>Le(min) CORREGIR A
δe= Le/2Rδe= 0.5θe=θe= 28.64788976θe=θe= 28.64788976Ae= (θe/3)-θex8.3x10^(-7)Ae= 9.549272808
B= θe-AeB= 19.09861695
Xe= Lex(1-((δe^2)/10)+((δe^4)/216)+((δe^6)/9360)+((δe^8)/685440))Xe= 14.6293654Ye= Lex(((δe^2)/3)+((δe^3)/42)+((δe^5)/1320)+((δe^7)/75600))Ye= 2.455710706
u=u= 10.13421711v=v= 5.122194186
P=P= 0.619449135K=K= 7.437982324
CURAVAS SIMETRICAS
Te=Te= 29.01276237αc= α-2θeαc= 50.89755382Lc= πxRx(αc/180)Lc= 13.32494843
Lc+2Le43.32494843
πxRx(α/180)+Le43.32494843
TE= PI-TeTE= 1+053.329EC= TE+LeEC= 1+068.329CE= EC+LeCE= 1+081.654ET= CE+LeET= 1+096.654ET= TE+LTET= 1+096.654
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)
180xδe/π
90xLe/πxR
Xe-(Ye/Tanθe)
Ye/(Senθe)
Ye-r(1-Cosθe)
Xe-R(Senθe)
(R+P)*Tg(α/2)+K
LT=LT=LT=LT=
S= 3.063619116 m/mP= (V^2/(127xR))-fP= 0.24808399 m/mP= 24.80839895 %
C H. IZQ. Nº15CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 48.168889 ˚PI= 1+155.097 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 62R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 52.1237539046
T= RxTan(α/2)T= 27.7137418142
E= Rx(Sec(α/2)-1)E= 5.91208644524
M= R-RxCos(α/2)
M= 5.39740978066597
Gc=Gc= 18.4825095203
Gc*l/20
21.2548859484
C=C= 22.86834366
CL=CL= 50.6022442373
θ/2
10.6274429742
Gc*l/40
10.6274429742
PC= PI-TPC= 1+127.383PT= PC+LcPT= 1+179.507
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 1.19772911623P= (V^2/(127xR))-fP= 0.192500635 m/mP= 19.2500635001 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. DER. Nº 16CALCULO DE LOS ELEMENTOS ESPIRAL CURVA ESPIRAL
DATOS DE DISEÑO
V(Diseño)= 25 Km/hRc= 30 mα= 60.46694444 ˚PI= 1+248.811 m.A= 25n= 2
ANCH0 VIA= 6 m.
REQUERIMIENTO DE UTILIZACION DE CURVAS DE TRANSICIÓN:
0.098xV^261.25SI NECESITA CURVAS DE TRANSICIÓN
CALCULOS
Le(min)= (0.036xV^3)/RLe(min)= 18.75
A= (Le*R)^0.5Le= (A^2)/R
RMT=
RMT=
RMT>Rc
Le= 20.83333333Le>Le(min) Ok
δe= Le/2Rδe= 0.347222222θe=θe= 19.89436789θe=θe= 19.89436789Ae= (θe/3)-θex8.3x10^(-7)Ae= 6.63143945
B= θe-AeB= 13.26292844
Xe= Lex(1-((δe^2)/10)+((δe^4)/216)+((δe^6)/9360)+((δe^8)/685440))Xe= 20.58356572Ye= Lex(((δe^2)/3)+((δe^3)/42)+((δe^5)/1320)+((δe^7)/75600))Ye= 2.390579918
u=u= 13.97763278v=v= 7.025184858
P=P= 0.60022736K=K= 10.37495214
CURAVAS SIMETRICAS
Te=Te= 28.20865011αc= α-2θeαc= 20.67820867Lc= πxRx(αc/180)Lc= 10.82708474
Lc+2Le52.49375141
πxRx(α/180)+Le52.49375141
TE= PI-TeTE= 1+220.602EC= TE+LeEC= 1+241.436CE= EC+LeCE= 1+252.263ET= CE+LeET= 1+273.096ET= TE+LTET= 1+273.096
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)
180xδe/π
90xLe/πxR
Xe-(Ye/Tanθe)
Ye/(Senθe)
Ye-r(1-Cosθe)
Xe-R(Senθe)
(R+P)*Tg(α/2)+K
LT=LT=LT=LT=
S= 1.628210946 m/mP= (V^2/(127xR))-fP= 0.084041995 m/mP= 8.404199475 %
C H. DER. Nº17CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 11.976944 ˚PI= 1+362.991 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 222.982R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 46.6115139511
T= RxTan(α/2)T= 23.3909944838
E= Rx(Sec(α/2)-1)E= 1.22351051868
M= R-RxCos(α/2)
M= 1.21683370692227
Gc=Gc= 5.1390497451
Gc*l/20
5.90990720686
C=C= 22.9898052896
CL=CL= 46.5266952621
θ/2
2.95495360343
Gc*l/40
2.95495360343
PC= PI-TPC= 1+339.600PT= PC+LcPT= 1+386.212
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 0.49097686785P= (V^2/(127xR))-fP= -0.036719155 m/mP= -3.6719155044 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. DER. Nº18CALCULO DE LOS ELEMENTOS CURVA CIRCULAR
DATOS DE DISEÑO
V(Diseño)= 50 Km/hα= 23.624444 ˚PI= 1+415.405 m.
f= 0.315e= 0.04
l(Cons C)= 23n= 2
ANCH0 VIA= 6 m.
CALCULOS
R(min)= V^2/(127x(e+f)R(min)= 55.450815127
R(asum)= 62R(asum)>R(min) Ok
Lc= πxRxα/180Lc= 25.5641090496
T= RxTan(α/2)T= 12.9662783819
E= Rx(Sec(α/2)-1)E= 1.34133228057
M= R-RxCos(α/2)
M= 1.31292788454077
Gc=Gc= 18.4825095203
Gc*l/20
21.2548859484
C=C= 22.86834366
CL=CL= 25.3834022978
θ/2
10.6274429742
Gc*l/40
10.6274429742
PC= PI-TPC= 1+402.439PT= PC+LcPT= 1+428.003
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)S= 1.19772911623P= (V^2/(127xR))-fP= 0.192500635 m/mP= 19.2500635001 %
360/(πxR)
θ=θ=
2xRxSen(θ/2)
2xRxSen(α/2)
ø=ø=ø=ø=
C H. IZQ. Nº 19CALCULO DE LOS ELEMENTOS ESPIRAL CURVA ESPIRAL
DATOS DE DISEÑO
V(Diseño)= 25 Km/hRc= 49 mα= 104.5538889 ˚PI= 1+592.373 m.A= 25n= 2
ANCH0 VIA= 6 m.
REQUERIMIENTO DE UTILIZACION DE CURVAS DE TRANSICIÓN:
0.098xV^261.25SI NECESITA CURVAS DE TRANSICIÓN
CALCULOS
Le(min)= (0.036xV^3)/RLe(min)= 11.47959184
A= (Le*R)^0.5Le= (A^2)/R
RMT=
RMT=
RMT>Rc
Le= 12.75510204Le>Le(min) Ok
δe= Le/2Rδe= 0.130154102θe=θe= 7.457280757θe=θe= 7.457280757Ae= (θe/3)-θex8.3x10^(-7)Ae= 2.485754063
B= θe-AeB= 4.971526694
Xe= Lex(1-((δe^2)/10)+((δe^4)/216)+((δe^6)/9360)+((δe^8)/685440))Xe= 12.73351174Ye= Lex(((δe^2)/3)+((δe^3)/42)+((δe^5)/1320)+((δe^7)/75600))Ye= 0.552707058
u=u= 8.510959023v=v= 4.25857212
P=P= 0.138260403K=K= 6.373951518
CURAVAS SIMETRICAS
Te=Te= 69.89858485αc= α-2θeαc= 89.63932737Lc= πxRx(αc/180)Lc= 76.6605687
Lc+2Le102.1707728
πxRx(α/180)+Le102.1707728
TE= PI-TeTE= 1+522.474EC= TE+LeEC= 1+535.230CE= EC+LeCE= 1+611.890ET= CE+LeET= 1+624.645ET= TE+LTET= 1+624.645
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)
180xδe/π
90xLe/πxR
Xe-(Ye/Tanθe)
Ye/(Senθe)
Ye-r(1-Cosθe)
Xe-R(Senθe)
(R+P)*Tg(α/2)+K
LT=LT=LT=LT=
S= 1.070144754 m/mP= (V^2/(127xR))-fP= 0.020433874 m/mP= 2.043387434 %
C H. IZQ. Nº 20CALCULO DE LOS ELEMENTOS ESPIRAL CURVA ESPIRAL
DATOS DE DISEÑO
V(Diseño)= 25 Km/hRc= 15 mα= 124.9986111 ˚PI= 1+677.573 m.A= 20n= 2
ANCH0 VIA= 6 m.
REQUERIMIENTO DE UTILIZACION DE CURVAS DE TRANSICIÓN:
0.098xV^261.25SI NECESITA CURVAS DE TRANSICIÓN
CALCULOS
Le(min)= (0.036xV^3)/RLe(min)= 37.5
A= (Le*R)^0.5Le= (A^2)/R
RMT=
RMT=
RMT>Rc
Le= 26.66666667Le>Le(min) CORREGIR A
δe= Le/2Rδe= 0.888888889θe=θe= 50.92958179θe=θe= 50.92958179Ae= (θe/3)-θex8.3x10^(-7)Ae= 16.97648499
B= θe-AeB= 33.9530968
Xe= Lex(1-((δe^2)/10)+((δe^4)/216)+((δe^6)/9360)+((δe^8)/685440))Xe= 24.63816474Ye= Lex(((δe^2)/3)+((δe^3)/42)+((δe^5)/1320)+((δe^7)/75600))Ye= 7.466365538
u=u= 18.5768122v=v= 9.616995841
P=P= 1.920491302K=K= 12.99258592
CURAVAS SIMETRICAS
Te=Te= 45.49558544αc= α-2θeαc= 23.13944753Lc= πxRx(αc/180)Lc= 6.057893198
Lc+2Le59.39122653
πxRx(α/180)+Le59.39122653
TE= PI-TeTE= 1+632.077EC= TE+LeEC= 1+658.744CE= EC+LeCE= 1+664.802ET= CE+LeET= 1+691.469ET= TE+LTET= 1+691.469
S= n(R-(R^2-L^2)^0.5)+(V/10x(R^0.5)
180xδe/π
90xLe/πxR
Xe-(Ye/Tanθe)
Ye/(Senθe)
Ye-r(1-Cosθe)
Xe-R(Senθe)
(R+P)*Tg(α/2)+K
LT=LT=LT=LT=
S= 3.063619116 m/mP= (V^2/(127xR))-fP= 0.24808399 m/mP= 24.80839895 %