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Stirling Dynamics is a recognised Industry leader in Loads and Aeroelastics. We have over 20 years experience providing whole aircraft loads for new and modification/upgrade programmes. Our engineers have extensive knowledge and experience of EASA, FAA and military standards and requirements, including standards for new and supplemental certification. We can provide a total solution, generating the aerodynamics, geometry, critical case identification, design loads and certification loads covering both static and fatigue. Whether it is small scale problem solving or research, or whole aircraft loads calculation - concept to certification - our engineers can advise you on the issues. Download Flyer
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Aeroelastics (Flutter)
Stirling is a world expert in Flutter Certification. We cover the full range of capabilities from model build to providing certification support, and lead programmes to support flutter certification clearance for civil and military aircraft. Our specialists provide the CVE function to a number of organisations holding DOA status under EASA Part 21J.
We supply a complete service from preliminary design assesment of the aero-structure, detailed modelling for development and validation, through ground and flight vibration testing and certificate submission.
Our portfolio includes:
- Small Aircraft flutter clearances for special payloads.
- Analyses for the Air Accident Investigation Branch.
- Roll control using wing twist.
- Rotor control by means of servo-flaps.
- Skynet launch loads structural verification.
Research Partnerships
Stilring has partnered with Airbus to manage their Loads and Aeroelastics research strategy under the DiPaRT initiative, providing the key interface between Airbus and its external research partners.
Loads and Aeroelastics Tool Set
Stirling has a suite of specialist software and processes to efficiently support aircraft programmes, both new and modifications.
| SD-GLOAD |
Landing gear and airframe response simulation package incorporating a post processing software to produce aircraft loads. Request more information
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| SD-APEX |
Allows the user to interactively create wing pressure maps over a user defined range of local lift coefficients. Request more information
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| SD-CLOAD |
Allows the calculation of wing component loads (i.e. leading and trailing edge devices, both retracted and deployed, and wing box) for full flight and ground loads conditions. Request more information
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| SD-Plot-EXY |
Rapid analysis and presentation of experimental and CFD force and pressure data. This is a general purpose 2D tool. Request more information
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Please contact us at Stirling US or Stirling UK for more information on our Loads and Aeroelastics capability.
Other Stirling Capabilities:
Landing Gear
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