Loading...
Please wait, while we are loading the content...
Similar Documents
Numerical calculation of the transonic potential flow past a cranked wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Tauber, M. Chang, I. C. |
| Copyright Year | 1983 |
| Description | The widely transonic swept-wing code, FL022, was found to have an error in the transformed flow equation in the computational domain. The revised version of the code correctly accounted for the non-straight leading edge geometry and its effect on the pressure distribution. |
| File Size | 3184248 |
| Page Count | 15 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840001982 |
| Archival Resource Key | ark:/13960/t0sr3q81d |
| Language | English |
| Publisher Date | 1983-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Flow Equations Transonic Flow Swept Wings Scaling Laws Pressure Distribution Supercritical Wings Mathematical Models Computer Programs Cartesian Coordinates Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |