1$STRESS\;of\;TENSION\;STEEL$
$(f_s)$
$f_s=\frac{600(d_t-c)}{c}
2BALANCED CONDITION
$c_b=\frac{600 \ d_t}{f_y+600}
3EQUILIBRIUM OF FORCES (SRB)
$0.85f'_c\,ab=A_sf_y
4NOMINAL MOMENT SRB
(RECTANGULAR SECTION)
$M_n=0.85f'_c\,ab\left(d-\frac{a}{2}\right)$
$M_n=A_sf_y\left(d-\frac{a}{2}\right)
5BALANCED STEEL RATIO
(RECTANGULAR SECTION)
$\rho_b=\frac{0.85{f'}_c\,\beta_1}{f_y}\left(\frac{600}{600+f_y}\right) \left(\frac{d_t}{d}\right)
6MAXIMUM STEEL RATIO
given
BALANCE STEEL RATIO
$\rho_{max}^{TC}= \dfrac{3}{8}\left(\frac{600+f_y}{600}\right) \rho_{bal}
7COEFFICIENT
of
RESISTING MOMENT
$R_n=\frac{M_u}{\phi\,bd^2}
8$\beta_1\ $
if
$\;{f'}_c >28MPa\,
$\beta_1=0.85-\frac{{0.05(f'}_c-28)}{7}
9FLEXURAL DESIGN STRENGTH
$M_u=\phi\rho\,f_ybd^2\left(1-\frac{\rho\;f_y}{1.7f_c^\prime}\right)
10$Maximum\ Moment$
$Tension-Controlled$
$(M_{umax\ T})$
$M_{umax\ T}\ =0.9\bullet\ \frac{3\ }{8}\left(0.85f_c'\ \beta_1\ bd^2\right)\left(1-\frac{3\ }{16}\beta_1\right)$
11$Maximum\ Moment$
$(M_{umax})$
$M_{umax\ }\ =\frac{49\ }{60}\bullet\ \frac{3\ }{7}\left(0.85f_c'\ \beta_1\ bd^2\right)\left(1-\frac{3\ }{14}\beta_1\right)$
12$f_s\le\,f_y$
$COMPRESSION\;CONTROLLED$
$\phi=0.65
13MINIMUM STEEL RATIO
$\rho_{min}=\frac{\sqrt{f'c}}{{4f}_y}$
$\rho_{min}=\frac{1.4}{f_y}\ $
14$f_s\geq\,f_y
$TENSION\;CONTROLLED$
$\varphi=0.90
15$f_y<f_s<1000MPa
$TRANSITION\;REGION$
$\phi=0.65+0.25\left(\frac{f_s-f_y}{1000-f_y}\right)
16EQUILIBRIUM OF FORCES (DRB)
$0.85f'_c\,ab+A'_s(f_s\;or\;f_y)=A_sf_y
17$STRESS\;of\;COMPRESSION\;STEEL\;$
$(f'_s)$
$f_s'=\frac{600(c-d')}{c}
18NOMINAL MOMENT DRB
(RECTANGULAR SECTION)
$M_n=0.85f'_c\,ab\left(d-\frac{a}{2}\right)$
$\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ +A'_s(f_s\;or\;f_y)(d-d')
19$DESIGN\; SHEAR \;ON \;BEAMS$
$V_u
$V_u=\phi(V_c+V_s)
20SHEAR STRENGTH OF CONCRETE
(SIMPLIFIED CALCULATION IN BEAMS)
$\downdownarrows w/o\;axial\downdownarrows$
$V_c=0.17\lambda\sqrt{{f'}_c}b_wd$
_________________________________
$\downdownarrows w/\;axial \downdownarrows$
$V_c=0.17\lambda\sqrt{{f'}_c}b_wd\left(1+\frac{N_u}{14A_g}\right)$
21w/o AXIAL COMPRESSION
SHEAR STRENGTH OF CONCRETE
(DETAILED CALCULATION IN BEAMS)
CHOOSE SMALLEST VALUE
$V_c=\left(\dfrac{1}{6}\lambda\sqrt{{f^\prime}_c}+17\rho_w\frac{V_ud}{M_u}\right)b_wd$
$V_c=\left(\dfrac{1}{6}\lambda\sqrt{{f^\prime}_c}+17\rho_w\right)b_wd$
$V_c=0.29\lambda\sqrt{{f'}_{c\ }}b_wd
22w/ AXIAL COMPRESSION
SHEAR STRENGTH OF CONCRETE
(DETAILED CALCULATION IN BEAMS)
CHOOSE SMALLEST VALUE
$V_c=\left(\dfrac{1}{6}\lambda\sqrt{{f^\prime}_c}+17\rho_w\frac{V_ud}{M_m}\right)b_wd$
$V_c=0.29\lambda\sqrt{{f'}_c}b_wd\sqrt{1+\frac{0.29N_u}{A_g}}
23w/ AXIAL TENSION
SHEAR STRENGTH OF CONCRETE
(DETAILED CALCULATION IN BEAMS)
$V_c=\ 0.17\ \lambda\ \sqrt{{f'}_c}{\ b}_w\ d\ \left(1+\frac{N_u}{3.5\ A_g}\right)$
24Relationship
SPACING and SHEAR
of Stirrups
$V_s\,\&\,S\;\;\;$
$\sigma=\frac{F}{A}$
$f_{yt}=\frac{V_s}{A_v(\frac{d}{S})}$
$S=\frac{A_vf_{yt}d}{V_s}
25$S_{max}$
if
$V_u>\phi\,V_c
$V_s\le0.33\sqrt{{f\prime}_c}\,\,b_w\,\,d$
$\ \ \ \ \ \ \ then\rightarrow\ \ \ \ \ \ \ {\ S}_{max}=\frac{d}{2}\ or\ 600$
_________________________________
$V_s\ >0.33\sqrt{{f\prime}_c}\,\,b_w\,\,d$
$\ \ \ \ \ \ \ then\rightarrow\ \ \ \ \ \ \ {\ S}_{max}=\frac{d}{4}\ or\ 300$
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26$S_{max}$
$\dfrac{1}{2}\phi\ V_c\le\,V_u\ <\phi\,V_c
$S_{max}=\frac{A_vf_{yt}}{0.062\; \sqrt{{f'c}}\; b_w}$
$S_{max}=\frac{A_vf_{yt}}{0.35b_w}
27MINIMUM SHEAR REINFORCEMENT AREA
$A_{vmin}=0.062\sqrt{f'c}\frac{b_w}{f_{yt}}S$
$A_{vmin}=0.35\frac{b_w}{f_{yt}}S
28PARAMETERS
SPACING
and
REINFORCEMENT AREA
for
$\dfrac{1}{2}\phi\ V_c\le\,V_u\ <\phi\,V_c$
$\dfrac{1}{2}\phi\ V_c\le\,V_u\ <\phi\,V_c$
$therefore $
$MINIMUM\ SHEAR$$REINFORCEMENT$$AREA$
29PARAMETERS OF SPACING
$\phi\,V_c<\,V_u
$\phi\,V_c< V_u $
therefore
$V_u=\phi\left(V_c+V_s\right)
30EFFECTIVE MOMENT OF INERTIA
$(I_e)$
$I_e=\left(\frac{M_{cr}}{M_{a}}\right)^3I_g+\left[1-\left(\frac{M_{cr}}{M_{a}}\right)^3\right]I_{cr}\le\ I_g$

31PARAMETERS OF SPACING
$\dfrac{1}{2}\phi\ V_c>\,V_u
$\dfrac{1}{2}\phi\ V_c>\,V_u\ $
$\therefore$
$S_{max}
32Ultimate Threshold Torque
Non-Prestressed Members
$T_{Uth}$
$T_{Uth}=0.75 \left(\frac{1}{12}\right) \lambda\ \sqrt{{f'}_c}\ \left(\frac{{A_{cp}}^2}{P_{cp}}\right)$

33Ultimate Threshold Torque
Prestressed Members
$T_{Uth}$
$T_{Uth}=0.75 \left(\frac{1}{12}\right)\ \lambda\ \sqrt{{f'}_c}\ \left(\frac{{A_{cp}}^2}{P_{cp}}\right)\ \sqrt{1+\frac{3f_{pc}}{ \lambda\ \sqrt{{f'}_c}\ }}$

34Ultimate Threshold Torque For Non-Prestressed Members
subjected to axial tensile or compression
$T_{Uth}$
$T_{Uth}=0.75 \left(\frac{1}{12}\right)\ \lambda\ \sqrt{{f'}_c}\ \left(\frac{{A_{cp}}^2}{P_{cp}}\right)\ \sqrt{1+\frac{3N_u}{\lambda\ A_g\ \sqrt{{f'}_c}\ }}$

35Cracking Torque
Non-Prestressed Members
$T_{cr}$
$T_{cr}=0.33\ \lambda\ \sqrt{{f'}_c}\ \left(\frac{{A_{cp}}^2}{P_{cp}}\right)$

36Cracking Torque
Prestressed Members
$T_{cr}$
$T_{cr}=0.33\ \lambda\ \sqrt{{f'}_c}\ \left(\frac{{A_{cp}}^2}{P_{cp}}\right)\ \sqrt{1+\frac{3f_{pc}}{ \lambda\ \sqrt{{f'}_c}\ }}$

37Cracking Torque Non-Prestressed Members
subjected to axial tensile or compression
$T_{cr}$
$T_{cr}=0.33\ \lambda\ \sqrt{{f'}_c}\ \left(\frac{{A_{cp}}^2}{P_{cp}}\right)\ \sqrt{1+\frac{3N_u}{ \lambda\ A_g\ \sqrt{{f'}_c}\ }}$

38Torsional Moment Strength
$T_n$
Lesser of the Two $T_n=\ \frac{2\ A_o\ A_t\ f_{yt}}{S}\ cot\theta$
$T_n=\ \frac{2\ A_o\ A_l\ f_{yt}}{P_h}\ cot\theta$

39$Additional\ $
$Longitudinal\ Reinforcement$
for Torsion
$A_l\ =\ P_h\frac{A_t\ }{S}\frac{f_{yt}\ }{f_y}\ {cot}^2\ \theta$
40Spacing of Torsional Reinforcement
$(S_{max})$
CHOOSE SMALLEST
300 or $\frac{P_h}{8}$
41If Torsional Reinforcement is Required,
minimum transverse reinforcement shall be the GREATER of
CHOOSE LARGERAt = area of one shear reinforcement
(one leg only). 
42Minimum Area of
Logitudinal Torsional Reinforcement
43SLENDERNESS EFFECT
is permitted to be
NEGLECTED
if
CONSIDERED AS
SHORT COLUMN
44CRACKING MOMENT
$(M_{cr})
$f_r=\ 0.62\lambda\sqrt{{f\prime}_c}\ =\ \frac{M_{cr}\ y_{tension}}{I_g}$
$f_r=\ 7.5\lambda\sqrt{{f\prime}_{c(psi)}}\ =\ \frac{M_{cr}\ y_{tension}}{I_g}$
45TWO WAY SLAB DISTRIBUTION
$trian\ to\ distd\ load=\ \frac{qs}{3}$
$trape\ to\ distd\ load=\ \frac{qs}{3}\ \left(\frac{3-\ m^2}{2}\right)$

46MODULUS of ELASTICITY (Ec)
$\left(w_c=\ 1440\ to\ 2560\ \frac{kg}{m^3}\right)$
$E_c=\ 0.043\ {w_c}^{1.5}\sqrt{{f'}_c}$
47MODULUS of ELASTICITY (Ec)
(normal wt. concrete)
$E_c=\ 4700\ \sqrt{{f'}_c}$
48LOADS used on FINDING the
SUSTAINED DEFLECTION
are SERVICE LOADS (NOT FACTORED)\*
LOADS used on FINDING the
SUSTAINED DEFLECTION
are SERVICE LOADS (NOT FACTORED)\*
49ADDITIONAL TIME DEPENDENT DEFLECTION
$=\delta_{sustained\ loads}\ *\ \lambda_\Delta$
$\lambda_\Delta=\frac{\xi}{1+\ 50\ \rho'}$
50EFFECTIVE MOMENT OF INERTIA
OF CONTINUOUS SLAB OR BEAM
$I_e^{conti}=\frac{I_e^{+critical}+I_e^{-critical}}{2}$

51(NSCP 2001 &2010)
INTERIOR T-BEAM
$b_f$
$b_f=\left[\begin{matrix}\frac{L}{4}\\b_w\ +\ 16\ t_f\\b_w\ +\ \ \frac{S_1}{2}+\frac{S_2}{2}\\\end{matrix}\right]$
52(NSCP 2001 &2010)
L-BEAM
$b_f$
$b_f=\left[\begin{matrix}b_w\ +\frac{L}{12}\\b_w\ +\ 6\ t_f\\b_w\ +\ \ \frac{S_1}{2}\\\end{matrix}\right]$
53(NSCP 2015)
L-BEAM
$b_f$
$b_f=\left[\begin{matrix}b_w\ +\frac{l_n}{12}\\b_w\ +\ 6\ t_f\\b_w\ +\ \ \frac{S_1}{2}\\\end{matrix}\right]$
54(NSCP 2015)
INTERIOR T-BEAM
$b_f$
$b_f=\left[\begin{matrix}\frac{l_n}{4}\\b_w\ +\ 16\ t_f\\b_w\ +\ \ \frac{S_1}{2}+\frac{S_2}{2}\\\end{matrix}\right]$
55MINIMUM THICKNESS
ONE-WAY SLAB and BEAM
USES CENTER to CENTER SPAN
56MINIMUM REINFORCEMENT
and
SHRINKAGE and TEMPERATURE BARS
for SLAB and FOOTING
57CALTECH
COLUMN
Plastic Centroid
with respect to created origin
58SPIRAL CIRCULAR COLUMN
$P_u=\ 0.75\ \left(0.85\right)\left(0.85\ {f'}_c\left(A_g-A_{st}\right)+A_{st}f_y\right)$
59TIED COLUMN
$P_u=\ 0.65\ \left(0.80\right)\left(0.85\ {f'}_c\left(A_g-A_{st}\right)+A_{st}f_y\right)$
60SPACING OF TIES
FOR TIED COLUMN
$(S_{max})$
choose smallest
$\frac{4}{3}A_g\ ,\ 16\ d_B\ ,\ 48\ d_{st}$
$and\ $
$Least\ Column\ Dimension$
61CODE
SHEAR CAPACITY
of
SPIRAL COLUMN
62COLUMNS
CONCRETE SHEAR CAPACITY
of
SPIRAL COLUMN
$V_c=\ \frac{1}{6}\lambda\ \sqrt{{f\prime}_c}\left(0.8D^2\right)$
63PERCENTAGE OF SPIRAL STEEL
or
VOLUMETRIC SPIRAL
REINFORCEMENT RATIO
(also applicable on seismic)
choose largest
$\rho_s=0.45\left(\frac{D^2}{{D_c}^2}-1\right)\frac{{f'}_c}{f_{yh}}$
$\rho_s=\dfrac{{0.12\ f'}_c}{f_{yh}}\ $
64PITCH (spacing of spiral)
$S\ =\ \frac{\pi\left(D_c-d_{st}\right)}{\rho_s}\left(\frac{d_{st}}{D_c}\right)^2$
65COLUMNS
ALLOWABLE CENTER to CENTER PITCH
(SPACING of CONTINUOUS BAR)
for
SPIRAL COLUMN
BETWEEN
$\frac{4}{3}A_{g\ }\ or\ \left(25mm+d_{st}\right)$
to
$\left( 75mm+d_{st}\right)$
66COLUMNS
$\rho_{max}\ \&\ \rho_{min}$
$Logitudinal\ Steel\ Percentage\ \ \left(\rho_g\right)$
for SPIRAL COLUMN
$\rho_{min}\ \ \ to\ \ \ \rho_{max}\ $
$0.01\ -\ \ 0.08$
67COLUMNS
$\rho_{max}\ \&\ \rho_{min}$
$Logitudinal\ Steel\ Percentage\ \ \left(\rho_g\right)$
for
TIED COLUMN
$\rho_{min}\ \ \ to\ \ \ \rho_{max}\ $
$0.02\ -\ \ 0.08$
68COLUMNS
MINIMUM NUMBER of LOGITUDINAL BARS
TIED COLUMN
4 BARS
4 BARS
4 BARS
69COLUMNS
MINIMUM NUMBER of LOGITUDINAL BARS
SPIRAL COLUMN
6 BARS
6 BARS
6 BARS
70EULER BUCKLING LOAD or
CRITICAL LOAD
$P_{c\ }=\ \frac{\pi^2\ \left(EI\right)_{eff}}{\left(kL_u\right)^2}$
71EFFECTIVE FLEXURAL RIGIDITY
$\left(EI\right)_{eff}$
$\left(EI\right)_{eff}=\ \frac{0.40\ E_c\ I_g}{1+\ \beta_{dns}}$
$\left(EI\right)_{eff}=\ \frac{0.20\ E_c\ I_g\ +\ E_s\ I_{se}}{1+\ \beta_{dns}}\ $
$\beta_{dns}\ =\frac{factored\ sustained\ load\ (usually\ DL)\ }{total\ factored\ load}$
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74COLUMN ALIGNMENT CHART
(JOINT RIGIDITY)
$\ G_{Above\ or\ Below}\ =\frac{\sum\left(\frac{EI}{L}\right)_{all\ conn.\ \ columns}}{\sum\left(\frac{EI}{L}\right)_{all\ conn.\ \ beams}}$

75SLENDER COLUMN
MOMENT MAGNIFICATION FACTOR
$\delta\ =\ \frac{C_m}{1\ -\frac{P_u}{0.75P_c\ }}\ \geq\ 1.00$

76CONCEPT
(ASD)
Singly Reinforced Beam
Uncracked Section
77CONCEPT
(ASD)
Singly Reinforced Beam
Cracked Section
78CONCEPT
(ASD)
Doubly Reinforced Beam
Cracked Section
79CONCEPT
(ASD)
Top and Bottom about N.A.
Static Moment Area are Equal
80CONCEPT
(ASD)
Transformed
Moment of Inertia
Moment of Inertia about N.A

81(ASD)
Stress in
Tension Steel
$\frac{f_s}{n}=\ \frac{M\ y_{sb}}{I_T}$

82(ASD)
Stress in
Compression Concrete
$f_c=\ \frac{M\ y_{c}}{I_T}$

83(ASD)
Stress in
Compression Steel
$\frac{f'_s}{2n}=\ \frac{M\ y_{st}}{I_T}$

84Modular Ratio
(n)
$\frac{E_s}{E_c}\geq\ 6$
85(ASD)
Allowable Bending
Stress in Concrete
$f_c=\ 0.45{f'}_c$
86(ASD)
Allowable Stress in Steel
$for\ G280\ \ steel\ \ \ \ \ \ \ \ \ f_s=\ 140\ MPa $
$for\ G420\ \ steel\ \ \ \ \ \ \ \ \ f_s=\ 170\ MPa$
87CONCEPT
BALANCE CONDITION
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92ALWAYS
$f_s\ = f_y$
FOR
SINGLY-REINFORCED BEAM (SRB)
ONE-WAY SLAB
FOOTINGS
ALWAYS
$f_s\ = f_y$
FOR
SINGLY-REINFORCED BEAM (SRB)
ONE-WAY SLAB
FOOTINGS
93SEISMIC LOGITUDINAL REINFORCEMENT
$\rho_{max}\ \&\ \rho_{min}$
$Logitudinal\ Steel\ Percentage\ \ \left(\rho_g\right)$
for
TIED COLUMN
$\rho_{min}\ \ \ to\ \ \ \rho_{max}\ $
$0.01\ -\ \ 0.06$
94SEISMIC HOOP REINFORCEMENT
Spacing
Hoop Reinforcement
EQUATE to S, and CHOOSE SMALLEST
$\frac{A_{sh}\ }{S\ \bullet\ b_c}\ =\ 0.3\ \left(\frac{D^2}{{D_c}^2}-1\right)\frac{{f'}_c}{f_{yt}}$
$\frac{A_{sh}\ }{S\ \bullet\ b_c}\ =\ 0.09\left(\frac{{f'}_c}{f_{yt}}\right)$
95SIDESWAY- UNINHIBITED
UNBRACED FRAME
SIDESWAY- PERMITTED
SWAY FRAME
96SIDESWAY- INHIBITED
BRACED FRAME
SIDESWAY- PREVENTED
NON-SWAY FRAME
97SEISMIC HOOP REINFORCEMENT
Maximum Spacing
Hoop Reinforcement
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100MAXIMUM STEEL RATIO
(TENSION CONTROLLED)
$\rho_{max}^{TC}$
$\rho_{max}^{TC}=\ \frac{0.85\ {f\prime}_c\ }{f_y}\ \bullet\beta_1\ \left(\frac{3}{8}\right)\ \left(\frac{d_t}{d}\right)$
101MAXIMUM STEEL RATIO
(TRANSITION REGION)
$\rho_{max}^{TR}$
$\rho_{max}^{TR}=\ \frac{0.85\ {f\prime}_c\ }{f_y}\ \bullet\beta_1\ \left(\frac{3}{7}\right)\ \left(\frac{d_t}{d}\right)$
102in DETERMINING the
MAXIMUM NUMBER of BARS
using $\rho_{max}$
ROUND DOWN to NEAREST WHOLE NUMBER of the obtain PIECES
in DETERMINING the
MAXIMUM NUMBER of BARS
using $\rho_{max}$
ROUND DOWN to NEAREST WHOLE NUMBER of the obtain PIECES
103MINIMUM STRAIN ALLOWED by the CODE
$\epsilon = 0.004$
to have
ALLOWABLE MAX REINFORCEMENT
TRANSITION CONTROLLED
MINIMUM STRAIN ALLOWED by the CODE
$\epsilon = 0.004$
to have
ALLOWABLE MAX REINFORCEMENT
TRANSITION CONTROLLED
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112IN EULER's CRITICAL AXIAL LOAD
$P_{cr}$
the WEAK MOMENT of INERTIA
with reduction factor
MUST be USED
in REINFORCED CONCRETE
IN
EULER's CRITICAL AXIAL LOAD$P_{cr}$
the
WEAK MOMENT of INERTIA with
reduction factor MUST be USEDin
REINFORCED CONCRETE
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118COMBINE SHEAR and TORSION REINFORCEMENT
$\left(\dfrac{A_v}{s}\right)^{combined}=\left(\dfrac{A_v}{s}\right)^{shear} + \left(\dfrac{A_t}{s}\right)^{torsion}$
_________________________
$\left(\dfrac{n A_b}{s_{req}}\right)=\left(\dfrac{A_v}{s_v}\right) + \left(\dfrac{n A_t}{s_t}\right)$
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