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Some effects of reynolds and mach numbers on the lift of an naca 0012 rectangular wing in the naca 19-foot pressure tunnel
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1943 |
| File Size | 5538747 |
| Page Count | 11 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092735 |
| Archival Resource Key | ark:/13960/t55f21p3s |
| Language | English |
| Publisher Date | 1943-01-01 |
| Access Restriction | Open |
| Subject Keyword | Mach Number Lift Coefficients - Airfoils - Naca 0012 Reynolds Number Wings, Rectangular - Characteristics Wind Tunnel Tests - Naca - Pressure (19') Air Flow - Compressibility 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 |