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. The cited research is consistent with the Under Secretary of Defense for Research and Engineering priority focus areas and the Army Modernization Strategy. Research in this Project is performed by the United States Army Futures Command.
Document Details
- Document Type
- Project
- Publication Date
- Oct 01, 2024
- Source ID
- CW5_0602183A_2_2040_PB_2024
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