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Effects of propellers and of vibration on the extent of laminar flow on the naca 27-212 airfoil
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1939 |
| File Size | 6070008 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092787 |
| Archival Resource Key | ark:/13960/t9380js8r |
| Language | English |
| Publisher Date | 1939-01-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution - Airfoils - Naca 27-212 Boundary Layer - Airfoils Laminar Wind Tunnel Tests - Naca - High-speed (8') Airfoils - Naca 27-212 Laminar-flow Boundary Layer Transition Airfoils - Naca - Laminar-flow 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 |