# Timber Beam-Column Design per NDS 2018 Using RF-/TIMBER AWC Module

### Technical Article

In this article, the adequacy of a 2x4 dimension lumber subject to combined bi-axial bending and axial compression is verified using RF-/TIMBER AWC add-on module. The beam-column properties and loading are based on example E1.8 of AWC Structural Wood Design Examples 2015/2018.

The member is a no. 2 Southern Pine, 2x4 nominal, 3 feet long and used as a truss member. Lateral support is provided only at the member ends and they are considered pinned. The dead (DL), snow (SL), and wind (WL) loads are applied at the top and mid-point of the beam-column, as shown below.

The member properties are shown after selecting the appropriate cross-section and material in the program.

#### Adjustment Factors Listed in Table 4.3.1 of NDS 2018 for ASD Design

The reference design values (F_{b}, F_{c}, and E_{min}) are multiplied by the applicable adjustment factors to determine the adjusted design values. For sawn lumber, these factors are found in Table 4.3.1 [1]. There are eleven different adjustment factors for the ASD design. Many of these factors are equal to 1.0 in the NDS example [2]. However, brief description and how RF-/TIMBER AWC accounts for each factor is given below.

#### Factors Calculated by the Program

C_{L} ... Beam Stability Factor. It depends on the geometry and lateral support of the member as described in section 3.3.3 [1]. This factor is automatically calculated in RF-/TIMBER. (Note: The effective length, le used to calculate C_{L} is defined by the user in the 'Effective Length' section of RF-/TIMBER AWC. The option "Acc. to Table 3.3.3" with the appropriate loading case must be selected). The image below shows the applicable loading case for this example.

C_{F} ... Size Factor. It depends on the depth and thickness of the member as specified in section 4.3.6 [1]. This factor is automatically determined in RF-/TIMBER AWC.

C_{fu} ... Flat Use Factor. It accounts for weak axis bending of the member as specified in section 4.3.7 [1]. This factor is automatically calculated in RF-/TIMBER AWC.

C_{P} ... Column Stability Factor. It depends on the geometry, end-fixity conditions, and lateral support of the member as described in section 3.7.1 [1]. When a compression member is fully supported throughout its length, C_{P} = 1.0. This factor is automatically calculated in RF-/TIMBER AWC for both strong and weak axis directions.

#### Factors Defined by User-Input

C_{D} ... Load Duration Factor. It accounts for various loading periods based on the load case such as dead, snow, and wind based on section 4.3.2 [1]. Selecting "ASCE 7-16 NDS (Wood)" as standard in RFEM activates the load duration option in the Load Cases dialogue box. The load duration class (Permanent, Ten Years, etc.) default setting is based on the 'Action Category' of the load case. This setting can be adjusted by the user in RFEM or RF-/TIMBER AWC. The value selected by the program is based on Table 2.3.2 [1].

C_{M} ... Wet Service Factor. It accounts for the moisture service conditions of the member as specified in section 4.1.4 [1]. The user can select "wet" or "dry" in the 'In-Service Conditions' section of RF-/TIMBER AWC.

C_{t} ... Temperature Factor. It accounts for exposure to elevated temperatures of up to 100 degrees F, 100 to 125, and 125 to 150 as described in section 2.3.3 [1]. The user can select between the three temperature ranges in the 'In-Service Conditions' section of RF-/TIMBER AWC. The value selected by the program is based on Table 2.3.3 of [1].

C_{i} ... Incising Factor. It accounts for the loss of the area from the small incisions made in the member to receive preservative treatment for decay prevention as described in section 4.3.8 [1]. The user can select "Not Incised" or "Incised" in the 'Additional Design Parameters' section of RF-/TIMBER AWC.

C_{r} ... Repetitive Member Factor. It is used when multiple members act compositely to properly distribute a load amongst themselves as described in section 4.3.9 [1]. C_{t} = 1.15 for members that meet the criteria of being closely spaced and connected by a sheathing or equivalent. The user can select "Not Repetitive" or "Repetitive" in the 'Additional Design Parameters' section of RF-/TIMBER AWC.

Note: If necessary, code-based values of the user-input adjustment factors can be changed in the 'Standard' option.

#### Factors excluded in the Program

C_{T} ... Buckling Stiffness Factor. It accounts for the contribution of plywood sheathing to the buckling resistance of compression truss chords as specified in section 4.4.2 [1]. This factor is used to increase E_{min} of the member. C_{T} can be manually calculated per equation 4.4-1 [1] or conservatively taken as 1.0.

C_{b} ... Bearing Area Factor. It is used to increase the compression design values (F_{cp}) for concentrated loads applied perpendicular to grain as specified in section 3.10.4 [1]. C_{b} can be manually calculated per equation 3.10-2 [1] or conservatively taken as 1.0.

#### Actual Stress in the Beam-Column

In this example, the load combination has been simplified to CO1: DL + SL + WL.

Compression stress from dead and snow load, f_{c} = 171 psi

Strong-axis bending stress from wind load, f_{bx} = f_{b1} = 353 psi

Weak-axis bending stress from dead and snow load, f_{by} = f_{b2} = 1,029 psi

#### Determine the Adjusted Design Values per NDS 2018 Table 4.3.1 ASD Method

Critical Buckling Design Value for Compression Member in Strong Axis, F_{cEx}

${\mathrm{F}}_{\mathrm{cEx}}={\mathrm{F}}_{\mathrm{cE}1}=\frac{0.822\xb7{\mathrm{E}}_{\mathrm{min}}\text{'}}{{\left[{\displaystyle \frac{{\mathrm{l}}_{\mathrm{e}1}}{{\mathrm{d}}_{1}}}\right]}^{2}}\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{cEx}}={\mathrm{F}}_{\mathrm{cE}1}=\frac{0.822\xb7510,000\mathrm{psi}}{{\left[{\displaystyle \frac{36.0\mathrm{in}}{3.5\mathrm{in}}}\right]}^{2}}\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{cEx}}={\mathrm{F}}_{\mathrm{cE}1}=3,963\mathrm{psi}$

F_{cEx} |
Critical buckling design value for compression member in strong axis, psi |

E_{min}' |
= E_{min} ⋅ C_{M} ⋅ C_{T} ⋅ C_{i} = 510,000 psi |

l_{e1} |
Effective length = 36.0 in |

d_{1} |
Depth of member = 3.5 in |

Critical Buckling Design Value for Compression Member in Weak Axis, F_{cEy}

${\mathrm{F}}_{\mathrm{cEy}}={\mathrm{F}}_{\mathrm{cE}2}=\frac{0.822\xb7{\mathrm{E}}_{\mathrm{min}}\text{'}}{{\left[{\displaystyle \frac{{\mathrm{l}}_{\mathrm{e}2}}{{\mathrm{d}}_{2}}}\right]}^{2}}\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{cEy}}={\mathrm{F}}_{\mathrm{cE}2}=\frac{0.822\xb7510,000\mathrm{psi}}{{\left[{\displaystyle \frac{36.0\mathrm{in}}{1.5\mathrm{in}}}\right]}^{2}}\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{cEy}}={\mathrm{F}}_{\mathrm{cE}2}=728\mathrm{psi}$

F_{cEy} |
Critical buckling design value for compression member in weak axis, psi |

E_{min}' |
= E_{min} ⋅ C_{M} ⋅ C_{T} ⋅ C_{i} = 510,000 psi |

l_{e2} |
Effective length = 36.0 in |

d_{2} |
Thickness of member = 1.5 in |

Adjusted Compressive Design Value Parallel to Grain, F_{c'}

${\mathrm{F}}_{\mathrm{c}}\text{'}={\mathrm{F}}_{\mathrm{cy}}\text{'}={\mathrm{F}}_{\mathrm{c}}\xb7{\mathrm{C}}_{\mathrm{D}}\xb7{\mathrm{C}}_{\mathrm{M}}\xb7{\mathrm{C}}_{\mathrm{t}}\xb7{\mathrm{C}}_{\mathrm{F}}\xb7{\mathrm{C}}_{\mathrm{i}}\xb7{\mathrm{C}}_{\mathrm{P}}\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{c}}\text{'}={\mathrm{F}}_{\mathrm{cy}}\text{'}=1,450\mathrm{psi}\xb71.6\xb71.0\xb71.0\xb71.0\xb71.0\xb70.29\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{c}}\text{'}={\mathrm{F}}_{\mathrm{cy}}\text{'}=673\mathrm{psi}$

F_{c'} |
Adjusted compressive design value parallel to grain, psi |

F_{c} |
Reference compressive design values parallel to grain, psi |

C_{D} |
Load duration factor |

C_{M} |
Wet service factor |

C_{t} |
Temperature factor |

C_{F} |
Size factor |

C_{i} |
Incising factor |

C_{P} |
Column stability factor |

Critical Buckling Design Value for Bending Member, F_{bE}

${\mathrm{F}}_{\mathrm{bE}}=\frac{1.20\xb7{\mathrm{E}}_{\mathrm{min}}\text{'}}{{{\mathrm{R}}_{\mathrm{B}}}^{2}}\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{bE}}=\frac{1.20\xb7510,000\mathrm{psi}}{{9.65}^{2}}\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{bE}}=6,577\mathrm{psi}$

F_{bE} |
Critical buckling design value for bending member, psi |

E_{min}' |
= E_{min} ⋅ C_{M} ⋅ C_{T} ⋅ C_{i} = 510,000 psi |

R_{B} |
Slenderness ratio = 9.65 < 50 (NDS equation 3.3-5) |

Adjusted Strong Axis Bending Design Value, F_{bx'}

${\mathrm{F}}_{\mathrm{bx}}\text{'}={\mathrm{F}}_{\mathrm{b}1}={\mathrm{F}}_{\mathrm{b}}\xb7{\mathrm{C}}_{\mathrm{D}}\xb7{\mathrm{C}}_{\mathrm{M}}\xb7{\mathrm{C}}_{\mathrm{L}}\xb7{\mathrm{C}}_{\mathrm{t}}\xb7{\mathrm{C}}_{\mathrm{F}}\xb7{\mathrm{C}}_{\mathrm{i}}\xb7{\mathrm{C}}_{\mathrm{r}}\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{bx}}\text{'}={\mathrm{F}}_{\mathrm{b}1}=1,100\mathrm{psi}\xb71.6\xb71.0\xb70.982\xb71.0\xb71.0\xb71.0\xb71.0\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{bx}}\text{'}={\mathrm{F}}_{\mathrm{b}1}=1,729\mathrm{psi}$

F_{bx'} |
Adjusted strong axis bending design value, psi |

F_{b} |
Reference bending design value, psi |

C_{D} |
Load duration factor |

C_{M} |
Wet service factor |

C_{L} |
Beam stability factor |

C_{t} |
Temperature factor |

C_{F} |
Size factor |

C_{i} |
Incising factor |

C_{r} |
Repetitive member factor |

Adjusted Weak Axis Bending Design Value, F_{by'}

${\mathrm{F}}_{\mathrm{by}}\text{'}={\mathrm{F}}_{\mathrm{b}2}={\mathrm{F}}_{\mathrm{b}}\xb7{\mathrm{C}}_{\mathrm{D}}\xb7{\mathrm{C}}_{\mathrm{M}}\xb7{\mathrm{C}}_{\mathrm{L}}\xb7{\mathrm{C}}_{\mathrm{t}}\xb7{\mathrm{C}}_{\mathrm{fu}}\xb7{\mathrm{C}}_{\mathrm{F}}\xb7{\mathrm{C}}_{\mathrm{i}}\xb7{\mathrm{C}}_{\mathrm{r}}\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{by}}\text{'}={\mathrm{F}}_{\mathrm{b}2}=1,100\mathrm{psi}\xb71.6\xb71.0\xb71.0\xb71.0\xb71.1\xb71.0\xb71.0\xb71.0\phantom{\rule{0ex}{0ex}}{\mathrm{F}}_{\mathrm{by}}\text{'}={\mathrm{F}}_{\mathrm{b}2}=1,936\mathrm{psi}$

F_{by'} |
Adjusted weak axis bending design value, psi |

F_{b} |
Reference bending design value, psi |

C_{D} |
Load duration factor |

C_{M} |
Wet service factor |

C_{L} |
Beam stability factor |

C_{t} |
Temperature factor |

C_{fu} |
Flat use factor |

C_{F} |
Size factor |

C_{i} |
Incising factor |

C_{r} |
Repetitive member factor |

Combined Bi-axial Bending and Axial Compression Design Ratio

Inserting the actual stresses and limiting design values presented above into NDS equation 3.9-3 [1], the final design ratio is shown below.

${\left(\frac{{\mathrm{f}}_{\mathrm{c}}}{{\mathrm{F}}_{\mathrm{c}}\text{'}}\right)}^{2}+\frac{{\mathrm{f}}_{\mathrm{bx}}}{{\mathrm{F}}_{\mathrm{bx}}\text{'}\xb7\left[1-\left({\displaystyle \frac{{\mathrm{f}}_{\mathrm{c}}}{{\mathrm{F}}_{\mathrm{cEx}}}}\right)\right]}+\frac{{\mathrm{f}}_{\mathrm{by}}}{{\mathrm{F}}_{\mathrm{by}}\text{'}\xb7\left[1-\left({\displaystyle \frac{{\mathrm{f}}_{\mathrm{c}}}{{\mathrm{F}}_{\mathrm{cEy}}}}\right)-{\left({\displaystyle \frac{{\mathrm{f}}_{\mathrm{bx}}}{{\mathrm{F}}_{\mathrm{bE}}}}\right)}^{2}\right]}\u2a7d1.0\phantom{\rule{0ex}{0ex}}{\left(\frac{171}{673}\right)}^{2}+\frac{353}{1,729\xb7\left[1-\left({\displaystyle \frac{171}{3,965}}\right)\right]}+\frac{1,029}{1,936\xb7\left[1-\left({\displaystyle \frac{171}{728}}\right)-{\left({\displaystyle \frac{353}{6,577}}\right)}^{2}\right]}=0.98$

f_{c} |
Compression stress from dead and snow load |

F_{c'} |
Adjusted compressive design value parallel to grain |

f_{bx} |
Strong-axis bending stress from wind load |

F_{bx'} |
Adjusted strong axis bending design value |

F_{cEx} |
Critical buckling design value for compression member in strong axis |

f_{by} |
Weak-axis bending stress from dead and snow load |

F_{by'} |
Adjusted weak axis bending design value |

F_{cEy} |
Critical buckling design value for compression member in weak axis |

F_{bE} |
Critical buckling design value for bending member |

And NDS equation 3.9-4 [1],

$\frac{{\mathrm{f}}_{\mathrm{c}}}{{\mathrm{F}}_{\mathrm{cEy}}}+{\left(\frac{{\mathrm{f}}_{\mathrm{bx}}}{{\mathrm{F}}_{\mathrm{bE}}}\right)}^{2}\le 1.0\phantom{\rule{0ex}{0ex}}\frac{171}{728}+{\left(\frac{353}{6,577}\right)}^{2}=0.24$

f_{c} |
Compression stress from dead and snow load |

F_{cEy} |
Critical buckling design value for compression member in weak axis |

f_{bx} |
Strong-axis bending stress from wind load |

F_{bE} |
Critical buckling design value for bending member |

#### Result in RF-/TIMBER AWC

The user can compare each adjustment factors and adjusted design values from the analytical hand calculation method to the result summary in RF-/TIMBER AWC. As shown, the results are identical. The controlling final design ratio = 0.98 is based on the geometrically linear analysis (1^{st} degree) calculation method. Keep in mind that the default setting in RFEM for the load combination is set to the second-order analysis. This will result in a slightly larger design ratio = 1.03. The user has the option to choose which method listed in the 'Calculation Parameters' is best for the structure.

#### Author

#### Cisca Tjoa, PE

Customer Support & Marketing

Cisca provides technical support for Dlubal Software customers and contributes to the marketing outreach throughout North America.

#### Keywords

Design Timber Column NDS AWC Beam-Column

#### Reference

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Separate Load Entry for Structure or Foundation Design

In RF-/FOUNDATION Pro, the foundation design requires the definition of the corresponding loading (load cases, load combinations, or result combinations) for the different design situations (STR, GEO, UPL, or EQU).

The cross-section resistance design analyzes tension and compression along the grain, bending, bending and tension/compression as well as the strength in shear due to shear force.

The design of structural components at risk of buckling or lateral-torsional buckling is performed according to the Equivalent Member Method and considers the systematic axial compression, bending with and without compressive force as well as bending and tension. Deflection of inner spans and cantilevers is compared to the maximal allowable deflection.

Separate design cases allow for a flexible and stability analysis of members, sets of members, and loads.

Design-relevant parameters such as the stability analysis type, member slendernesses, and limit deflections can be freely adjusted.

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