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Subsonic two-dimensional-flow conditions near an airfoil determined by static pressures measured at the tunnel wall
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 3977762 |
| Page Count | 46 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082550 |
| Archival Resource Key | ark:/13960/t20c99313 |
| Language | English |
| Publisher Date | 1949-04-01 |
| Access Restriction | Open |
| Subject Keyword | Cauchy's Law Air Flow Velocity, High - Subsonic Airfoils - Naca 66,2-215 - Low-drag Airfoils - Naca 66,2-015 - Low-drag Photography - Air Flow - Airfoils - Schlieren Method Wind Tunnel Wall Interference - Airfoils Pressure Distribution - Airfoils - Naca 0012 Wind Tunnel Tests - Naca - High-speed (18"x4") Air Flow - Airfoils - 2-dimensional 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 |