Working Group #2: Static Aeroelastic Deformation Working Group (with AePW)

Leads: Ben Rider, Stefan Keye, and Garrett McHugh

Fluid-structure interactions will be calculated and studied in detail. This group will be comprised of individuals in both DPW and AePW communities with significant collaboration leading up to the final workshop.

Meeting Information

March 21, 2025
February 21, 2025
January 17, 2025
November 15, 2024
October 18, 2024
September 20, 2024
August 16, 2024
July 19, 2024
June 21, 2024

Test Cases

Test Case 1
1a (Required): ONERA OAT15A transonic airfoil RANS validation
Link to experimental data
Detailed Information

1b (Required): CRM FEM validation
More information coming

Test Case 2
2a(E) (Required): Static CRM wing/body fluid-structure interaction at cruise condition CL=0.50
2b(E) (Required): Static CRM wing/body fluid-structure interaction for polar at M=0.85
Detailed Information 2a (Encouraged): Rigid analysis at AOA=2.50 deg of pre-deformed geometry (ETW measurements) for comparision with 2a(E)
2b (Encouraged): Rigid analysis for polar at M=0.85 of pre-deformed geometry (ETW measurements) for comparision with 2b(E)
Detailed Information

Test Case 3

3: Static CRM wing/body/nacelle/pylon fluid-structure interaction
More information coming

Additional Test Cases
To be determined

NASA Official Responsible for Content

Brent W. Pomeroy

NASA Official Responsible for Content
Brent W. Pomeroy

Last Updated
January 17, 2025