Nonlinear Aerodynamic ROM - Structural ROM Methodology for Inflatable Aeroelasticity in Hypersonic Atmospheric Entry

Project: Research project

Project Details

StatusFinished
Effective start/end date1/25/087/24/08

Funding

  • National Aeronautics Space Administration (NASA): $31,545.00

Fingerprint

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.