Services
Our team provides services to different aircraft models and support early design stages to the certified vehicle.
- Structural Static and Dynamic Loads Analyses
- FAA Loads and Flutter DER (14 CFR Part 23 and 25)
- Flight, ground, landing, maneuver and gust.
- External (nacelles, fairings, antennae, struts, inlets, etc.)
- Loads flight test validation
- Aeroelastic Analyses
- Whirl flutter analysis
- Flight flutter testing
- Ground Vibration Test (GVT) support and analysis.
- Finite Element Analysis (FEA)
- Aerodynamic design of aircraft modifications, such as radomes and fairings
- Stability and control
- Critical conditions for aerodynamic loads
- Supply of mapped pressure data for FEM analysis
- Calculation of impact of modifications on aircraft performance
- Aerodynamic induced vibrations assessments
- Design and Analysis:
- Cooling and ventilation system
- Icing accretion and ice shedding
- Aero-optical analysis
- Calculation of field of regard for antennas and sensors
- Lighting obscuration analysis
- 14 CFR 25.571(e) birdstrike analysis
- Propeller design and analysis
- Preliminary weight estimates
- Weight-CG envelope definition
- Weight & Balance design support
- Weight & Balance documentation and certification
- Ground and fight test
- GVT and flight flutter test
- Flight loads survey
- FAA Aircraft Loads and Flutter DER
(14 CFR Part 23 and 25) - Certification plans
- TC & STC certification documents
- FAA DER Approval
Unit Members at several ODA’s
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FAA certification – Part 25 and Part 23
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Military certification
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Passenger to freighter conversion
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Special Mission Aircraft analysis, testing and certification
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Computational Fluid Dynamics (CFD) analysis
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Weight and Balance
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Flutter analysis and testings
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Structural loads analyses
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