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Inverse transonic airfoil design methods including boundary layer and viscous interaction effects (Document No: 19840013446)
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carlson, L. A. |
| Copyright Year | 1984 |
| Description | This report covers the period 1 September 1983 to 31 January 1984. The primary task during this reporting period was the continued development of the massive separation model and computer code (SKANSEP). In particular, detailed investigations were conducted with the boundary layer displacement surface correction technique discovered near the end of the last reporting period. This report will present detailed results using this technique and show comparisons with experimental data. |
| File Size | 846709 |
| Page Count | 37 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19840013446 |
| Archival Resource Key | ark:/13960/t18m24w4r |
| Language | English |
| Publisher Date | 1984-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Incompressible Flow Turbulence Wind Tunnel Tests Airfoils Angle of Attack Boundary Layers Displacement Computer Programs Viscous Flow Lift Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
