Loading...
Please wait, while we are loading the content...
Similar Documents
On the calculation of supersonic, separating, and reattaching flows. [boundary layer equations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Murphy, J. D. Presley, L. L. Rose, W. C. |
| Copyright Year | 1975 |
| Description | A method is developed for solving the laminar and turbulent compressible boundary-layer equations for separating and reattaching flows. Results of this method are compared with experimental data for two laminar and three turbulent boundary-layer, shock-wave interactions. Several Navier-Stokes solutions were obtained for each of the laminar boundary-layer, shock-wave interactions considered. Comparison of these solutions indicates a first-order sensitivity in C sub f to the computational mesh selected in both the viscous and inviscid portions of the flow. |
| File Size | 1077318 |
| Page Count | 25 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760002926 |
| Archival Resource Key | ark:/13960/t4cp1wd4n |
| Language | English |
| Publisher Date | 1975-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Supersonic Flow Numerical Analysis Laminar Boundary Layer Turbulent Boundary Layer Shock Wave Interaction Separated Flow Boundary Layer Equations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
