Experimental and Computational Aeromechanics Tech
Abstract
This Project investigates new high fidelity computational methods to simulate aerodynamic effects and test methods of emerging rotorcraft lift technologies that could be incorporated into Future Vertical Lift (FVL) designs and other Army and Department of Defense (DoD) aviation systems. Research in this Project is fully coordinated with PE 0603043A (Air Platform Advanced Technology). The cited research is consistent with the Under Secretary of Defense for Research and Engineering priority focus areas and the Army Modernization Strategy. Work in this Project is performed by Aviation & Missile Center (AvMC).
Document Details
- Document Type
- Project
- Publication Date
- Oct 01, 2025
- Source ID
- CW5_0602183A_2_2040_PB_2025
Related Documents
- Root: Air Platform Applied Research
- Child Accomplishment: Experimental Aeromechanics
- Child Accomplishment: Computational Aeromechanics