Research Subcategory

Off-Design, Iced, and Actively Forced Wings

This research examines wing behavior in conditions where baseline aerodynamic assumptions no longer hold. The work spans ice-accreted airfoils, actively blown wings, and dynamically pitching delta wings with leading-edge-vortex control, all of which push the flow into regimes shaped by separation, contamination, actuation, or rapid motion. Rather than treating these cases as minor perturbations of a clean wing, the studies show that off-design conditions reorganize the flow in fundamental ways, changing coherent structures, wake development, vortex stability, and the relationship between geometry and performance.

Infographic

Research infographic

NotebookLM-generated infographic and video assets for this research subcategory. Click any image to open the full-size file, or play videos directly on the page.

Advancing Urban Air Mobility Aerodynamics infographic
Advancing Urban Air Mobility Aerodynamics
Future Aerodynamic Design
Contributors

Students who contributed to this work

Students connected to the publications and projects represented on this page.

Publications

Research publications in this area

Publication entries include citation details and student contributors where available.

Blown Wing Aerodynamic Coefficient Predictions Using Traditional Machine Learning And Data Science

Students

Student contributors are listed where available.

Citation
  • Blown Wing Aerodynamic Coefficient Predictions Using Traditional Machine Learning And Data Science. 2021.

Low Reynolds Number Experimental Aerodynamic Verification Of Scaled And Lewice Simulated Ice

Students

Student contributors are listed where available.

Citation
  • Low Reynolds Number Experimental Aerodynamic Verification Of Scaled And Lewice Simulated Ice. 2022.

Experimental Investigation of Dynamic Pitching Effects on a Delta Wing with Blown Jet

Students
Citation
  • Pabon, Julian A., and Sidaard Gunasekaran. "Experimental Investigation of Dynamic Pitching Effects on a Delta Wing with Blown Jet." In AIAA SCITECH 2026 Forum, p. 0285. 2026. https://doi.org/10.2514/6.2026-0285