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Effects of upper surface modification on the aerodynamic characteristics of the naca 63 sub 2-215 airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Hicks, R. M. Schairer, E. T. |
| Copyright Year | 1979 |
| Description | An upper surface modification designed to increase the maximum lift coefficient of a 63 sub 2 - 215 airfoil section was tested at Mach numbers of 0.2, 0.3, and 0.4 Reynolds numbers of 1.3 x 1 million, 2 x 10 sub 6 and 2.5 x 1 million. Comparisons of the aerodynamic coefficients before and after the modification were made. The upper surface modification increased the maximum lift coefficient of the airfoil significantly at all conditions. |
| File Size | 1326740 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790005853 |
| Archival Resource Key | ark:/13960/t9479696r |
| Language | English |
| Publisher Date | 1979-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Aerodynamic Configurations Airfoil Profiles Lift Drag Ratio Reynolds Number Aerodynamic Coefficients Surface Geometry Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
