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Aeroelastic analysis for aeropropulsion applications
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bakhle, Milind A. Keith Jr., Theo G. |
| Copyright Year | 2002 |
| Description | Aeroelastic codes with advanced capabilities for modeling flow require substantial computational time. On the other hand, fast-running linear aeroelastic codes lack the capability to model three-dimensional, transonic, vortical, and viscous flows. The goal of this work was to develop an aeroelastic code with accurate modeling capabilities and small computational requirements. |
| File Size | 745931 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20020034911 |
| Archival Resource Key | ark:/13960/t7cs0s25w |
| Language | English |
| Publisher Date | 2002-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Transonic Flow Three Dimensional Flow Computational Fluid Dynamics Computerized Simulation Aircraft Engines Aeroelasticity Computer Programs Viscous Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
