Engineering Analysis Report - Public Summary (Redacted)

Fluid-Structure Interaction (FSI) of the Bonded Aluminium Starlink Roof Mount on a Fibreglass Roof - Category 5 Wind

Prepared for: Air Vision Systems
Date: 10 April 2026
Version: Public summary v1.0 (redacted)
Air Vision Systems | Public Summary (Redacted)AVS logo
This document is a redacted public summary intended for website publication. Detailed CFD/FEA model inputs, material property datasets, mesh strategy, solver settings, pressure fields, full contour ranges, and adhesive product identifiers are intentionally withheld to protect Air Vision Systems intellectual property. A full technical report may be provided to verified partners under NDA.

Contents:

  1. 1. Purpose and scope
  2. 2. Wind loading basis (public)
  3. 3. Bonding approach (public)
  4. 4. Key outcomes (high-level)
  5. 5. Selected figures (redacted)
  6. 6. Conclusion and limitations

1. Purpose and scope

This public summary describes a one-way fluid-structure interaction (FSI) assessment of a low-profile aluminium Starlink roof mount bonded onto a fibreglass vehicle roof under extreme aerodynamic loading. It gives a transparent, high-level overview of the engineering work without disclosing proprietary modelling detail.

2. Wind loading basis (public)

The mount was assessed at a Category 5 equivalent wind speed of 275 km/h, evaluated at 0, 45 and 90 degree yaw angles. The 45 degree (quartering) case produced the worst-case localised loading and was used to set the safety limits. Detailed pressure fields and full contour ranges are withheld.

3. Bonding approach (public)

The mount uses a dual-adhesive bond combining a structural acrylic foam tape with a structural silicone to transfer aerodynamic loads into the fibreglass vehicle roof. Specific adhesive product identifiers and full material property datasets are withheld.

4. Key outcomes (high-level)

5. Selected figures (redacted)

The figure below illustrates a representative output. Detailed CFD pressure fields, meshing images, and full contour ranges are intentionally excluded.

Illustrative total-deformation contour of the bonded aluminium Starlink roof mount on a fibreglass roof under peak aerodynamic loading, showing localised deflection concentrated at the centre
Figure A: Illustrative total-deformation contour under peak aerodynamic loading.

6. Conclusion and limitations

The analysis confirms the bonded aluminium mount on a fibreglass roof is structurally sound under 275 km/h aerodynamic loading. The dual-adhesive configuration transfers the dynamic loads into the vehicle roof without exceeding material limits, with a substantial safety margin. Achieving this performance depends on correct surface preparation during installation. This public summary omits detailed model construction, material datasets, meshing, solver controls, and pressure mapping; it is general guidance and not a substitute for project-specific engineering sign-off.

Full technical report available under NDA.
The complete engineering report, including detailed calculation data, modelling assumptions, source figures, appendices and supporting technical evidence, may be made available to approved AVS partners, wholesalers, installers, commercial customers and authorised review parties under a signed non-disclosure agreement.