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Global flowfield about the v-22 tiltrotor aircraft (Document No: 19950020828)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Meakin, Robert L. |
| Copyright Year | 1995 |
| Description | The Chimera overset grid method is reviewed and discussed in the context of a method of solution and analysis of unsteady three-dimensional viscous flows. The state of maturity of the various pieces of support software required to use the approach is discussed. A variety of recent applications of the method is presented. Current limitations of the approach are identified. |
| File Size | 1254326 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19950020828 |
| Archival Resource Key | ark:/13960/t1sf7pz43 |
| Language | English |
| Publisher Date | 1995-03-23 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Three Dimensional Flow Computational Fluid Dynamics Technology Assessment Flow Distribution Computerized Simulation Unsteady Flow Computational Grids Grid Generation Mathematics Computer Programs Viscous Flow V-22 Aircraft Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |