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Effect of mach number on position error as applied to a pitot-static tube located 0.55 chord ahead of an airplane wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1944 |
| File Size | 6776524 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930093486 |
| Archival Resource Key | ark:/13960/t3cz6f898 |
| Language | English |
| Publisher Date | 1944-01-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnels - Naca - High-speed (2 Feet) (amer ) Effect OF Compressibility Airfoils - Thickness Wind Tunnel Tests - Naca - High-speed (2 Feet) Airfoils - Naca 16-106 Airfoils - Naca 16-130 Instruments - Pitot-static Tubes - Position Airfoils - Naca 16-215 Airfoils - Characteristics Mach Number 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 |