'A New CFD Approach for the Computation of General Rotorcraft Flows' The computation of rotary wing aerodynamics by Computational Fluid dynamics is very difficult because of the dominance of the vortical wake. Not only is the wake region very large and in
|Effective start/end date||9/1/08 → 1/26/11|
- National Aeronautics and Space Administration: $193,294.00
Explore the research topics touched on by this project. These labels are generated based on the underlying awards/grants. Together they form a unique fingerprint.