Calculation Package — Permit Submission For Authority Having Jurisdiction
ZS-2026-001-CALC-001 · Calculations for Permit

Polar-Zonohedron
Polyurethane-Foam Dome Structural Calculation Package

Stamped engineering calculations for permit submission per IBC 2024 / ASCE 7-22. Limit-state verification of a 5.63 m × 3.82 m, 73-panel rigid-PU-foam zonohedron.

Project
Zomes office prototype (ZS-2026-001)
Site address
to be entered by Owner / EOR
AHJ
per site address
Risk Category
II (ASCE 7-22 Tbl. 1.5-1)
Occupancy (IBC)
Group B / U — confirm with AHJ
Construction type
To be classified by AHJ — out of scope
Document No.
ZS-2026-001-CALC-001
Revision
0
Status
For permit submission
Date issued
2026-05-04
Prepared by
Shereef Bishay
Sheets
see Index
Engineer of Record — Stamp & Approval for Permit Awaiting wet seal & signature
Name (printed)   Firm   License No. / State / Expiration  
Signature & Date   Project address   Permit application No. (to be filled by AHJ)  
Engineer's wet seal & signature
this seal certifies the calculations within this package are reviewed and approved for permit submission

Companion document — engineering review report (index.html) — contains methodology, source-data deep-links, and reconciliation between independent analysis methods. The engineering review report is prepared for the EOR as their working document; this calculation package is the deliverable to the AHJ.

Index of Calculations

Calculations performed in this package.

Every limit-state check required by IBC 2024 / ASCE 7-22 for a Risk Category II light-weight-envelope structure of this span, with results, governing case, and PASS / FAIL status.

§CalculationReferenceSheet
2.0Codes & standardsIBC 2024 §1605, ASCE 7-22 Ch. 1, 2, 7, 26-302
3.0Geometry & material dataQSW26030006 (lab); ASTM D1621/D790/C273/D16233
4.0Loads — Dead, Snow, WindASCE 7-22 §7.3, §26.10, §27.3, §30.44
5.0Load combinationsASCE 7-22 §2.4 (ASD)5
6.0Plate-bending capacity checkTimoshenko & W-K Tbl. 86
7.0Joint-tension & joint-shear capacityASTM D1623 / C273 lab values7
8.0Membrane compression at baseEquilibrium8
9.0Local panel bucklingSS plate, k = 4 (Timoshenko)9
10.0Global shell snap-throughSpherical-cap (Timoshenko)10
11.0Foundation bearing pressureTotal reaction / footprint11
12.0Deflection serviceabilityIBC Tbl. 1604.312
13.0Conclusion of calculations13
14.0Limitations of this package13
15.0Engineer-of-Record stamp14
Codes & Standards

Governing codes in force.

ReferenceTitle / clause
IBC 2024 §1605Adopts ASCE 7-22 by reference
ASCE 7-22 Ch. 2Combinations of loads (ASD §2.4)
ASCE 7-22 Ch. 7Snow loads (§7.3 balanced; §7.6.1 unbalanced curved roof)
ASCE 7-22 §26.5–26.10Wind speed, exposure, velocity-pressure coefficients
ASCE 7-22 §27.3 / Fig. 27.3-2Domed-roof MWFRS pressures
ASCE 7-22 §30.4 / Fig. 30.4-7 / Tbl. 30.4-1Components & cladding
ASCE 7-22 Tbl. 1.5-1, 1.5-2Risk category (II); importance factors
IBC 2024 Tbl. 1604.3Deflection serviceability limits
ASTM D1621-16 (2023)Compressive properties — rigid cellular plastics
ASTM D790-17Flexural properties — plastics
ASTM C273/C273M-20Shear properties — sandwich-core materials
ASTM D1623-17 (2023)Tensile / tensile-adhesion — rigid cellular plastics
ASTM D1622-20Apparent density — rigid cellular plastics
APA Y510LIndustry-analogue safety factor (FoS = 2.5)
QSW26030006Material test certificate — Nanjing Guocai Testing, May 2026
Geometry & Material Data

Structural geometry and lab-tested allowables.

3.1 Geometry

Footprint diameter (mean)5.63 m
Apex height3.82 m
Equivalent spherical-cap radius R = (D²/4 + H²)/(2H)2.95 m
Number of structural panels73 (70 rhombic + 3 door framing)
Panel thickness t (uniform)76.2 mm (3.0 in)
Largest panel — Type 1 (governs plate bending)edge 1012 mm, diags 1414 × 1410 mm, area 1.025 m²
Polar symmetryN = 9
Foundation9 perimeter curb panels at grade — encastre BC in analysis

3.2 Material — Zomes PU foam (240 kg/m³)

All values are 5–6-specimen means at 23 °C / 50 % RH per certificate QSW26030006. Each row cites the controlling ASTM method. ↓ Download original certificate (PDF, 1.0 MB).

PropertySymbolValueTest method
Compressive strength (Y)σc2.47 MPaASTM D1621
Compressive modulus (Y)Ec72.2 MPaASTM D1621
Flexural strength (X)σb2.17 MPaASTM D790
Flexural modulus (X)Eb62.8 MPaASTM D790
Shear strength (parent, Y)τp0.649 MPaASTM C273
Joint shear strengthτj0.410 MPaASTM C273
Joint tensile strengthσt,j0.270 MPaASTM D1623
Apparent densityρ240 kg/m³ASTM D1622
Poisson's ratio (assumed)ν0.30

3.3 Allowables at FoS = 2.5

Allowable = laboratory ultimate ÷ FoS. The factor of safety is the SIP industry analogue per APA Y510L.

Limit stateUltimate (MPa)Allowable (MPa)
Plate bending2.170.868
Compression (membrane)2.470.988
Joint shear0.4100.164
Joint tension0.2700.108
Parent shear0.5840.234
Loads

Design loads per ASCE 7-22.

4.1 Dead load

D = ρ · t · g
  = 240 kg/m³ × 0.0762 m × 9.81 m/s²
  = 179.4 N/m²  (≈ 0.180 kPa, ≈ 3.75 psf)

Total dead reaction at foundation: 9.8 kN over the perimeter ring (9 base panels).

4.2 Snow load (ASCE 7-22 §7.3)

Two site presets are envelope-checked: baseline CONUS and severe.

ParameterSymbolBaselineSevere
Ground snowpg1.44 kPa (30 psf)4.79 kPa (100 psf)
Exposure factorCe1.001.00
Thermal factorCt1.001.00
Importance factorIs1.001.00
Flat-roof snowpf = 0.7 Ce Ct Is pg1.005 kPa3.352 kPa
Unbalanced peak (curved)pu ≈ 2 pf2.01 kPa6.70 kPa

4.3 Wind load (ASCE 7-22 §26.10, §27.3, §30.4)

ParameterSymbolBaselineSevere
Basic wind speed (3-s gust, Risk Cat II)V115 mph160 mph
Exposure categoryCD
Velocity-pressure exposure coefficientKz0.851.03
Topographic factorKzt1.001.00
Directionality factorKd1.001.00
Ground-elevation factorKe1.001.00
Velocity pressureqz = 0.00256 Kz Kzt Kd Ke1.38 kPa (28.8 psf)3.23 kPa (67.5 psf)

Net design wind pressures on panel surface

ActionGCppnet baselinepnet severe
MWFRS uplift (top zone)−0.99−1.42 kPa−3.33 kPa
MWFRS inward (windward)+0.40+0.55 kPa+1.29 kPa
C&C peak suction−2.78 (incl. GCpi)−3.83 kPa−8.98 kPa
C&C peak inward+1.68+2.31 kPa+5.43 kPa
Load Combinations

ASCE 7-22 §2.4 ASD combinations applied.

C1.   D
C2.   D + L
C3.   D + (L_r or S or R)
C4.   D + 0.75 L + 0.75 (L_r or S or R)
C5.   D + (0.6 W or 0.7 E)
C6.   D + 0.75 L + 0.75 (0.6 W) + 0.75 (L_r or S or R)
C7.   0.6 D + 0.6 W
C8.   0.6 D + 0.7 E

Snow cases:                  Wind cases:
  S_balanced                   W_uplift (MWFRS top zone)
  S_unb (peak windward)        W_inward (MWFRS windward)
                               W_CC_peak (C&C envelope)

Roof live L_r and rain R taken as zero for the dome geometry.
Seismic E retained but non-governing (D/C < 0.10) for this lightweight envelope.
Plate-Bending Capacity

Timoshenko SS rect-plate, worst panel (Type 1).

6.1 Method

Per Timoshenko & Woinowsky-Krieger Tbl. 8 (simply-supported rectangular plate, uniform pressure):

σ_b,demand = β · p · b² / t²        with β interpolated from b/a at ν = 0.30

Type-1 panel:  edge = 1012 mm, diags = 1414 × 1410 mm
               inscribed rect.: 1384 × 1407 mm,  b = 1384 mm,  a = 1407 mm
               aspect b/a = 0.984  →  β ≈ 0.0479  (Tbl. 8, ν = 0.30)
               t = 76.2 mm

6.2 Worst-case demand and capacity

Combop (kPa)σb,demand (MPa)σb,allow (MPa)D/CStatus
D + L (baseline)+0.180.1100.8680.13PASS
D + Sbalanced (baseline)+1.180.1150.8680.13PASS
D + Sunb (severe)+6.880.6640.8680.77PASS
D + Winward (severe)+1.470.5410.8680.62PASS
1.2D + 1.6S (severe)+5.580.5380.8680.62PASS
0.6D + Wuplift,CC (severe) — governing−9.090.8570.8680.99PASS — borderline
0.9D + 1.0Wuplift (severe)−9.070.8510.8680.98PASS

Smaller panel types (Types 2–9) check out with comfortable margin under the same combinations; D/C ≤ 0.50 throughout. See the engineering review report § VIII for the full per-type matrix. Type 1, governing combination, severe site: D/C = 0.99 (PASS at FoS = 2.5).

Joint Capacity

Joint shear and tension at panel-to-panel bond.

7.1 Demand model

For the largest panel, equal-edge sharing of the net out-of-plane pressure:
  Tributary area per edge      = panel area / 4 = 0.256 m²
  Edge force per unit length   = p · 0.256 / 1.012 m = p · 0.253 m  (kN/m)
  Bond cross-section per edge  = edge × thickness = 1.012 × 0.0762 = 0.0772 m²
  σ_t,demand                   = (p · 0.256) / 0.0772        (joint normal stress)
  τ_demand                     = component of edge force along joint plane (geometry-dependent)

7.2 Worst-case results (severe site)

Limit stateUltimate (MPa)Allow (FoS 2.5)Demand (MPa)D/CStatus
Joint tension (hand calc — 0.6D + Wuplift)0.2700.1080.02870.27PASS
Joint shear (hand calc — 0.6D + Wuplift)0.4100.1640.02870.18PASS
Joint tension (FE per-triangle p99)0.2700.1080.02760.26PASS
Joint shear (FE per-triangle p99)0.4100.1640.03560.22PASS

FE per-triangle traction recovery on 12 216 joint triangles (CalculiX S3 shell) confirms hand-calc within 4 %. Worst joint D/C = 0.27 (PASS). The conservative uniform-envelope C&C-peak recovery gives 0.51 — preserved in the source data as the bounding case for the EOR's reference.

Membrane Compression at Foundation Ring

Total vertical reaction over base-panel cross-section.

Total vertical (severe, 1.2D + 1.6S):  ≈ 94 kN
Base ring:                              9 panels, t × edge bond ≈ 0.0772 m² each
σ_c,demand                            =  94 / (9 × 0.0772 m²)  ≈  0.135 MPa
σ_c,allow (FoS 2.5)                   =  0.988 MPa
D/C                                   =  0.135 / 0.988  =  0.14         [PASS]
Local Panel Buckling

Classical SS plate buckling, k = 4.

σ_cr  =  4 π² E_b  /  [ 12 (1 − ν²) ]  · (t/b)²
      =  4 π² · 62.8 / [ 12 · 0.91 ] · (0.0762 / 1.012)²
      =  1.16 MPa
σ_demand (severe, D + W_uplift)   =  0.41 MPa
D/C                               =  0.35                                [PASS]
Global Shell Snap-Through

Spherical-cap critical stress, R = 2.95 m, t = 76.2 mm.

σ_cr  =  2 E (t/R)² / √( 3 (1 − ν²) )
      =  2 · 70.8 · (0.0762 / 2.95)² / √( 3 · 0.91 )
      =  0.057 MPa  (compressive)
σ_demand (apex membrane)           =  0.003 MPa
D/C                                =  0.05                               [PASS]

FE eigenvalue buckling on the merged volume mesh produced inconsistent results owing to mesh-quality artefacts (documented in the engineering review report § VII R4); the hand-calc spherical-cap result governs in this package.

Foundation Bearing Pressure

Total vertical reaction over footprint.

Footprint area                           ≈  25 m²
Total vertical (severe, 1.2D + 1.6S)     ≈  146 kN
σ_bearing                                =  146 / 25 = 5.8 kPa
σ_bearing,allow (typical, AHJ to confirm) =  100 kPa
D/C                                      =  0.06                          [PASS]

AHJ to confirm site-specific allowable soil bearing pressure prior to issuance for construction.

Deflection Serviceability

IBC Tbl. 1604.3 limits applied to span = 5.63 m.

Load case|u|max (mm)Limit (mm)D/CStatus
Dead6.915.6 (L/360)0.44PASS
D + Sbalanced14.723.5 (L/240)0.63PASS
0.6D + Wuplift (MWFRS)10.931.3 (L/180)0.35PASS
0.6D + WCC,peak envelope32.531.3 (L/180)1.04marginal — see note

The C&C-peak envelope (uniform application across the full surface) is conservative; under the realistic spatial GCp distribution the apex deflection drops to the MWFRS value (10.9 mm). EOR to confirm acceptance.

Conclusion

Summary of compliance.

Compliance statement

The structure described in this calculation package satisfies all short-term limit-state checks required by IBC 2024 / ASCE 7-22 at the project default factor of safety FoS = 2.5 across both the baseline (V = 115 mph, pg = 30 psf, Exposure C) and severe (V = 160 mph, pg = 100 psf, Exposure D) site envelopes. The governing limit state is plate bending of the largest panel under load combination 0.6D + Wuplift,CC at D/C = 0.99 (PASS, borderline). All other limit states pass with D/C ≤ 0.77.

13.1 Worst-case summary

Limit stateD/CGoverning comboStatus
Plate bending0.990.6D + Wuplift,CCPASS — borderline
Joint tension (hand calc)0.270.6D + WupliftPASS
Joint tension (FE p99 envelope, conservative)0.51wind C&C peak (uniform)PASS
Joint shear0.22wind C&C peak (FE p99)PASS
Local panel buckling0.29D + SPASS
Compression (membrane)0.151.2D + 1.6SPASS
Foundation bearing0.061.2D + 1.6SPASS
Global shell snap-through (hand calc)0.05D + SPASS
Deflection serviceability (MWFRS)0.63D + SbalancedPASS
Limitations of This Calculation Package

Items outside the scope of this submission.

Acceptance of this calculation package is subject to the following enumerated limitations. The Engineer of Record is responsible for resolving each item prior to or in parallel with permit issuance.

  1. Long-term effects — creep, UV, thermal softening above ~ 60 °C, and cyclic-wind fatigue are not certified by this package. Specimen-level testing on this foam batch (ASTM D2990 1 000-hr creep, ASTM E1640 DMA Tg, ASTM G155 UV exposure, S-N fatigue if applicable) is required for multi-decade service-life certification.
  2. Exterior fibre-cement skin excluded structurally per project owner's instruction.
  3. Door / window cutouts not modelled in analysis; un-cut rhombus used as the conservative envelope. Cut-panel detailing per the architectural shop drawings.
  4. Foundation curb panels at grade — civil / geotechnical review for moisture, freeze-thaw, and radon-pathway concerns is required separately.
  5. Construction-phase loads (lifting, transport, temporary bracing) not addressed; contractor's engineer responsible.
  6. Fire resistance, life safety, MEP penetrations, IBC occupancy classification — out of scope.
  7. Soil bearing pressure assumed at 100 kPa; AHJ to confirm.
  8. Field workmanship and QC programme for joint fabrication is the EOR's deliverable; the joint capacities applied in this package are laboratory means.
Engineer-of-Record Stamp

Final stamp and submission for permit.

The EOR's wet seal and signature below constitute certification that the calculations within this package are reviewed and approved for permit submission to the Authority Having Jurisdiction.

Engineer of Record — Final Stamp for Permit Submission Awaiting wet seal & signature
Name (printed)   Firm   License No. / State / Expiration  
Signature & Date   Project address   Permit application No. (AHJ)  
Engineer's wet seal & signature
(this page is the official submission to the AHJ; wet seal supersedes the "Awaiting" status on the cover)