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Investigation of boundary-layer reynolds number for transition on an naca 65(215)-114 airfoil in the langley two-dimensional low-turbulence pressure tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 10567429 |
| Page Count | 24 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082393 |
| Archival Resource Key | ark:/13960/t5s79q610 |
| Language | English |
| Publisher Date | 1948-10-01 |
| Access Restriction | Open |
| Subject Keyword | Drag, Profile - Measurement, Momentum Pressure Distribution - Airfoils - Naca 65 (215)-114 Boundary Layer Transition - Airfoils Reynolds Number Wind Tunnel Tests - Naca - Pressure, Low-turbulence Work Carried On At Lal ( 7 1 Airfoils - Naca 65 (215)-114 - Char & Ordinates Low-drag 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 |