Loading...
Please wait, while we are loading the content...
Similar Documents
Boundary-layer transition on the n.a.c.a. 0012 and 23012 airfoils in the 8-foot high-speed wind tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1940 |
| File Size | 18758085 |
| Page Count | 38 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092775 |
| Archival Resource Key | ark:/13960/t5t75m570 |
| Language | English |
| Publisher Date | 1940-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Tests - Naca - High-speed (8') Pressure Distribution - Airfoils - Naca 0012 Pressure Distribution - Airfoils - Naca 23012 Boundary Layer Transition - Wings Skin Friction - Airfoils Airfoils - Naca 23012 - Characteristics Airfoils - Naca 0012 - Characteristics 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 |