Bombardier Global Express
TAG was responsible for the stress analysis of the lightweight potable water tank. Finite element modeling ensured high quality results, optimizing the tank shape to conform to a specific design envelope.
Bombardier CRJ-700
TAG generated Damage Tolerance Analysis reports for numerous crack propagation sites in the cockpit airframe structure to develop inspection interval criteria.
SAAB-SCANIA AB, JAS 39A Griffin
Magnus Axelsson performed stress analysis and Finite Element Modeling, as well as damage tolerance analysis of primary and secondary aircraft structure, including advanced composites. He also analyzed conventional materials and full-height Honeycomb components for the Main Wing, Fin and Canard Wing. The resulting design delivered superior mission performance, as well as significant weight savings.
Bombardier RJ-50
Rob Moore was involved in the stress analysis of primary structure for the horizontal stabilizer. He was also responsible for the creation of a finite element model of this structure, which resulted in significant weight savings and overall structural design optimization.
Aeritalia, Naples
Mike Hurworth successfully completed a Finite Element Modeling of the passenger door structure for the ATR 72 to confirm a major design modification.
Contact us to find out how the TAG team can apply their considerable expertise to your analysis requirements.
AG has developed in-depth knowledge of aircraft airframe structures through many years of diverse project experience. Extensive experience with computer aided engineering software, as well as traditional analytical methods, means minimal redesign work, consistently high quality results and cost effectiveness for our customers. Finite Element Modeling software saves labour and expenses by allowing early detection and elimination of potential problem areas prior to physical testing, with little impact on budget or schedule.
Stress Analysis
