Register to access content

Please complete the form below to access content. All required fields are indicated with an *

Texas AM University: FSI simulation of an aircraft wing

Texas A&M researchers analyze aircraft wing slat with super-elastic SCF using CFD and FSI, addressing mesh challenges for noise reduction.

Researchers at Texas A&M University are conducting CFD (Computational Fluid Dynamics) and FSI (Fluid‑Structure Interaction) analyses of an aircraft wing leading edge slat that uses a Slat Cove Filler (SCF), made from a super-elastic shape memory alloy, to reduce aeroacoustic noise when the slat is deployed. Grid management challenges were encountered because the compression of the filler can cause mesh elements to go to zero volume. The CFD software needs to handle complex mesh deformations, non-linear materials, and facilitate the FSI analysis. Initial results show the computational and experimental results compare well.

Download the case study to find out more.

Contact information

Enquiry details

Privacy

Our Privacy Notice describes how we process Personal Data about you. It also provides information on how you may exercise any of your rights as a Data Subject. You have the right to withdraw your consent at any time by clicking on the "Unsubscribe" link within the electronic marketing communications sent to you. By submitting this form, you agree to our Terms of Use.

Our Privacy Notice describes how we process Personal Data about you. It also provides information on how you may exercise any of your rights as a Data Subject. You have the right to withdraw your consent at any time by clicking on the "Unsubscribe" link within the electronic marketing communications sent to you. By submitting this form, you agree to our Terms of Use.

*Required fields