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Preliminary report on laminar-flow airfoils and new methods adopted for airfoil and boundary-layer investigations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1939 |
| Description | Recent developments in airfoil-testing methods and fundamental air-flow investigations, as applied to airfoils, are discussed. Preliminary test results, obtained under conditions relatively free from stream turbulence and other disturbances, are presented. Suitable airfoils and airfoil-design principles were developed to take advantage of the unusually extensive laminar boundary layers that may be maintained under the improved testing conditions. The results are of interest mainly in range of below 6,000,000. |
| File Size | 2691850 |
| Page Count | 58 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092782 |
| Archival Resource Key | ark:/13960/t0cv7q21j |
| Language | English |
| Publisher Date | 1939-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Naca 27-209-char , A C , Moments, C P & Ord -laminar-flow Pressure Distribution - Airfoils - Naca Airfoils - Naca 27-215-char , A C , Moments, C P & Ord - Laminar-flow Airfoils - Naca - Char & Ord - Laminar-flow Airfoils - Naca 27-212-char , A C , Moments, C P & Ord -laminar-flow Boundary Layer - Airfoils - Laminar 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 |