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A theoretical method for the analysis and design of axisymmetric bodies. [flow distribution and incompressible fluids
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Beatty, T. D. |
| Copyright Year | 1975 |
| Description | A theoretical method is presented for the computation of the flow field about an axisymmetric body operating in a viscous, incompressible fluid. A potential flow method was used to determine the inviscid flow field and to yield the boundary conditions for the boundary layer solutions. Boundary layer effects in the forces of displacement thickness and empirically modeled separation streamlines are accounted for in subsequent potential flow solutions. This procedure is repeated until the solutions converge. An empirical method was used to determine base drag allowing configuration drag to be computed. |
| File Size | 11457050 |
| Page Count | 281 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750011517 |
| Archival Resource Key | ark:/13960/t7np6v27d |
| Language | English |
| Publisher Date | 1975-03-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Boundary Layer Separation Flow Distribution Inviscid Flow Boundary Conditions Separated Flow Incompressible Fluids Axisymmetric Bodies Viscous Flow Boundary Layer Flow Axisymmetric 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 |
