Classical Stress Analysis
Static and fatigue analysis of metal and composite airframe structures, from preliminary sizing through formal documentation and MRB support.
Aerospace Engineering Consulting
Oread Technical delivers classical stress analysis, finite element modeling, and program leadership for commercial, defense, and business aircraft programs.
Founded by Jeremy deNoyelles, Oread Technical provides multi-discipline aerospace engineering support across all phases of aircraft development — from preliminary design through fleet sustainment.
With leadership experience managing teams of up to 14 engineers and deep hands-on expertise in metal and composite structures, Oread Technical helps programs move from analysis to released drawings with confidence.
End-to-end structural engineering support for demanding aerospace programs.
Static and fatigue analysis of metal and composite airframe structures, from preliminary sizing through formal documentation and MRB support.
FEM development and survey using NASTRAN, PATRAN, ANSYS, and FEMAP for load path verification, buckling, and fleet issue resolution.
Excel-based pre-processors, optimization routines, and composite laminate theory tools that accelerate analyst workflows and reduce rework.
Team management, SOW/BOE development, design review presentations, supplier coordination, and earned value management as a certified CAM.
Analysis of frames, stringers, nacelle and thrust reverser structures using customer and in-house tools including ISAMI and laminate theory methods.
Structural support for conversions, flight test installations, cargo modifications, and ongoing fleet sustainment programs.
Representative programs across commercial, defense, and business aviation.
Lead — Floors Stress Team. Manage 13 stress engineers; define configurations with suppliers and customers; present PDR/CDR to program management.
Senior analyst surveying GFEM elemental stresses to resolve fleet issues for the remaining B-1B fleet.
Managed multi-discipline and stress teams (12–14 engineers) through prototype development, analysis, drawing release, and SDRL delivery. Two VP of Engineering Special Achievement Awards.
Led winglet and wing reinforcement analysis for Challenger and Global programs; formal documentation for Safety of Flight on C-Series installations.
Composite frame analysis (ISAMI), Excel automation for Airbus tools, BR725 nacelle/TRU structures, and pylon side skin fatigue analysis.
777, 767, 757, 737, and 747 floor and pylon structures. Developed PATRAN/NASTRAN optimization routines achieving substantial weight savings on 777 cargo floors.
Whether you need a lead stress engineer, a managed analysis team, or specialized tool development — reach out to discuss scope, timeline, and clearance requirements.