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Analytical study of subsonic turbulent boundary layer separation including viscous-inviscid interaction
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Inger, G. R. |
| Copyright Year | 1974 |
| Description | The prediction of boundary layer deceleration and separation in regions of adverse pressure gradients are discussed as an unsolved problem of fundamental practical importance in aerodynamics. A three layered theoretical flow model of boundary layer separation including viscous-inviscid interaction was conceived for the case of subsonic two dimensional steady laminar flow. |
| File Size | 1318023 |
| Page Count | 48 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750004182 |
| Archival Resource Key | ark:/13960/t20c9qr8z |
| Language | English |
| Publisher Date | 1974-11-30 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Boundary Layer Separation Turbulent Flow Algorithms Turbulent Boundary Layer Inviscid Flow Mathematical Models Perturbation Viscous Flow Pressure Gradients 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 |
