Structural analysis

Fink Roof Truss — Member Forces and NDS Check, Worked Example

By Michael Flynn, PE · water resources & dam safety engineer ·

A standard residential roof truss, start to finish: turning roof pressures into panel-point loads, solving the member forces by the method of joints, and checking the 2x6 chords and 2x4 webs to the NDS with the right load-duration factor for each combination. Two results surprise most people: dead load alone governs the bottom chord, and the short 2x4 webs can use less than a quarter of their crushing strength because they buckle about the narrow face.

The truss

TypeFink (W), 28 ft span, 6/12 pitch, trusses at 24 in on center
Loads (horizontal projection)TCLL 20 psf snow, TCDL 10 psf, BCDL 10 psf, BCLL 0
LumberDouglas Fir-Larch No. 2: 2x6 top and bottom chords, 2x4 webs (NDS Supplement Table 4A: Fb 900, Ft 575, Fc 1350, Emin 580,000 psi)
BracingTop chord sheathed, bottom chord ceiling-braced, webs unbraced out of plane
Combinations (ASD)D (CD = 0.9) and D + S (CD = 1.15)

Every number below comes straight out of the free calculator with its default inputs.

Open the truss calculator →
Fink truss member forces: top chords in compression up to 1,826 lb, bottom chord in tension up to 1,633 lb
Service D + S member forces in lb. Blue = tension, red = compression. Joints are numbered 1–4 along the bottom chord from the left, then 5, 6 (apex), 7 along the top.
Step 1 · Geometry

Rise, panel points and member lengths

Rise h = (L/2)(6/12) = 14 × 0.5 = 7.0 ft   tanθ = 0.5, sinθ = 0.4472, cosθ = 0.8944
Bottom chord joints at third points: x = 0, 9.333, 18.667, 28 ft
Top chord joints at quarter points: (7, 3.5), (14, 7.0), (21, 3.5) ft
Top chord panels = 7/cosθ = 7.826 ft   Short webs 2–5, 3–7 = 4.206 ft   Long webs 2–6, 3–6 = 8.413 ft
Step 2 · Panel-point loads

Tributary length × spacing × pressure

Top chord: (10 + 20) psf × 2 ft = 60 plf   (D 20 plf + S 40 plf)
Bottom chord: 10 psf × 2 ft = 20 plf
Top joints 5, 6, 7 take 7 ft each → D 140 lb + S 280 lb = 420 lb
Heel joints take 3.5 ft of top chord + 4.667 ft of bottom chord → D 163.3 lb + S 140 lb
Bottom joints 2, 3 take 9.333 ft → D 186.7 lb
Total = 60 × 28 + 20 × 28 = 2,240 lb  →  R = 1,120 lb each end
Heel loads go straight into the bearing. The 303 lb applied at each heel joint is part of the reaction but never passes through a member. Divide the whole roof load by the interior panel points and every member force comes out about 14% high.
Step 3 · Method of joints at the heel

The two biggest forces in the truss

Net upward force at joint 1 = 1,120 − 163.3 − 140 = 816.7 lb
ΣFy = 0: F1-5 sinθ = 816.7 → F1-5 = 816.7 / 0.4472 = 1,826 lb compression
ΣFx = 0: F1-2 = 1,826 × 0.8944 = 1,633 lb tension

Working inward joint by joint (or letting the calculator do it) gives the full set:

MemberJointsSizeD only (lb)D + S (lb)NDS ratioGoverns
Bottom chord, heel panels1–2, 3–42x6+793+1,6330.454D + S, tension + bending
Bottom chord, center panel2–32x6+529+1,0890.381D alone, tension + bending
Top chord, heel panels1–5, 7–42x6−887−1,8260.473D + S, compression + bending
Top chord, apex panels5–6, 6–72x6−809−1,5910.455D + S, compression + bending
Short webs2–5, 3–72x4−126−3790.181D + S, compression (CP = 0.223)
Long webs2–6, 3–62x4+351+6030.116D + S, tension

Check: the reactions sum to 2,240 lb, and the truss is determinate (m + r = 11 + 3 = 14 = 2j).

Step 4 · Top chord, compression + bending

NDS Eq. 3.9-3, member 1–5, D + S

fc = 1,826 / 8.25 in² = 221.3 psi
Fc* = Fc CD CF = 1350 × 1.15 × 1.10 = 1,707.8 psi
In-plane le/d = 7.826 × 12 / 5.5 = 17.08 (sheathing braces the weak axis)
FcE = 0.822 Emin / (le/d)² = 0.822 × 580,000 / 17.08² = 1,635.1 psi
CP (Eq. 3.7-1, c = 0.8, α = 0.9575) = 0.6758 → Fc′ = 1,154.1 psi
Panel moment M = w·Δx²/8 = 60 × 7² / 8 = 367.5 lb-ft → fb = 4,410 / 7.5625 = 583.1 psi
Fb′ = Fb CD CF Cr = 900 × 1.15 × 1.3 × 1.15 = 1,547.3 psi
(fc/Fc′)² + fb / [Fb′(1 − fc/FcE)] = 0.0368 + 0.4359 = 0.473 ≤ 1.0 ✓
Bending, not axial load, sizes this chord. Over 90% of the interaction comes from the panel moment. Checking the top chord as an axial member alone would show 0.19 and invite a 2x4 that fails. The panel moment here uses a simple span between panel points. ANSI/TPI 1 analyzes the chord as continuous, which lowers the midspan moment and adds moment over the panel points.
Step 5 · Why dead load alone governs the bottom chord

Member 2–3, tension + bending, NDS Eq. 3.9-1

Ceiling load bends the chord: M = 20 × 9.333² / 8 = 217.8 lb-ft → fb = 345.6 psi in both combinations
D (CD 0.9): ft/Ft′ + fb/Fb′ = 64.1/672.8 + 345.6/1,210.9 = 0.381
D + S (CD 1.15): 132.0/859.6 + 345.6/1,547.3 = 0.377

Snow adds axial tension, but it doesn't add ceiling bending, and the higher load-duration factor raises every allowable stress by 28%. The permanent ceiling load at CD = 0.9 ends up slightly worse. This is why the NDS has you check each combination with its own CD, rather than only the heaviest load at the shortest duration.

Step 6 · The short web and out-of-plane buckling

Member 2–5, 2x4, 4.21 ft, compression 379 lb

Unbraced out of plane: le/d = 4.206 × 12 / 1.5 = 33.65 (narrow face governs)
FcE = 0.822 × 580,000 / 33.65² = 421.0 psi; Fc* = 1350 × 1.15 × 1.15 = 1,785.4 psi
CP = 0.223 → Fc′ = 398.1 psi; fc = 379 / 5.25 = 72.1 psi → 0.181

A 2x4 web carries less than a quarter of its crushing capacity because it buckles about the 1.5 in face. The 8.4 ft long webs are in tension under gravity, so slenderness doesn't hurt them, until wind uplift reverses them. See the wind-uplift example.

Step 7 · Deflection

Pin-jointed elastic estimate

Max joint deflection, D + S = 0.097 in = L/3,466   Snow only = 0.048 in = L/6,934

That is far inside L/240 and L/360. Real metal-plate-connected trusses deflect more, because of plate slip at the joints and creep under sustained load. Truss design software adds both. Treat the pin-jointed number as a lower bound.

Tools used in this example

Truss calculator (default inputs), with the truss member force coefficients card for a quick hand check. To put the truss on a girder or a header, carry the reactions into the continuous beam or beam deflection tool.

Frequently asked questions

What are the member forces in a 28 ft Fink truss?

For a 28 ft, 6/12 Fink truss at 24 in on center with 20 psf snow, 10 psf top chord dead and 10 psf bottom chord dead load, the heel top-chord panels carry 1,826 lb compression and the heel bottom-chord panels carry 1,633 lb tension. The short webs carry 379 lb compression and the long webs 603 lb tension. Each reaction is 1,120 lb.

Why is a roof truss top chord checked for bending?

The roof sheathing loads the top chord along its whole length, not just at the panel points, so each top-chord panel bends between joints while it carries axial compression. In a typical residential truss, the bending stress is several times the axial stress, and the NDS combined-stress equation, not the axial check, sizes the chord.

Which load duration factor applies to roof truss design?

Each load combination is checked with the C_D of its shortest-duration load: 0.9 for dead load alone, 1.15 for snow, 1.25 for roof live load and 1.6 for wind. Because a lower C_D can govern, dead load alone is always one of the checks.

Get future worked examples in your inbox

One real design problem per month, with the math worked out and the gotchas called out. Free.

Free. Unsubscribe anytime. Privacy.