Loading...
Please wait, while we are loading the content...
Similar Documents
The effects of variations in reynolds number between 3.0 x 10 to the power 6 and 25.0 x 10 to the power 6 upon the aerodynamic characteristics of a number of naca 6-series airfoil sections
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 32670867 |
| Page Count | 44 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082445 |
| Archival Resource Key | ark:/13960/t4qk1rh6c |
| Language | English |
| Publisher Date | 1948-12-01 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Naca 631-012 - Char & Ordinates Airfoils - Naca 64-009 - Char & Ordinates Airfoils - Naca 64-006 - Char & Ordinates Airfoils - Naca 63-006 - Char & Ordinates Airfoils - Naca 63-009 - Char & Ordinates Reynolds Number Airfoils - Naca 631-212 - Char & Ordinates Airfoils - Naca 6-series - Char & Ordinates Airfoils - Naca 63-209 - Char & Ordinates Airfoils - Naca 633-018 - Char & Ordinates 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 |