Loading...
Please wait, while we are loading the content...
Similar Documents
Numerical solution for unsteady sonic flow over thin wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Wu, J. M. Kimble, K. R. |
| Copyright Year | 1974 |
| Description | A numerical solution precedure of a simplified unsteady transonic equation which is fast, reasonably accurate, and takes into account many of the effects of the steady flow field is described. The numeric solution of this equation is accurate and is accomplished on an IBM 360/65 computer. Arbitrary planform shape is accommodated and variable local Mach number effects from the steady flow are easily handled. |
| File Size | 831136 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750004827 |
| Archival Resource Key | ark:/13960/t8pc7rt3z |
| Language | English |
| Publisher Date | 1974-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Flow Equations Planforms Transonic Flow Steady Flow Flow Distribution Thin Wings Unsteady Flow Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
