Loading...
Please wait, while we are loading the content...
Similar Documents
The effects of amount and type of camber on the variation with mach number of the aerodynamic characteristics of a 10-percent-thick naca 64a- series airfoil section
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1950 |
| File Size | 2460526 |
| Page Count | 68 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082803 |
| Archival Resource Key | ark:/13960/t01z8j660 |
| Language | English |
| Publisher Date | 1950-05-01 |
| Access Restriction | Open |
| Subject Keyword | Wind Tunnel Tests - Aal - High-speed (3 1/2'x1') Airfoils - Naca 64a610 - Char , Moments & Ordinates Low-drag Airfoils - Naca 64a010 - Char , Moments & Ordinates Low-drag Airfoils - Naca 641610(a=0 4) - Char , Moments & Ordiantes Low-drag Airfoils - Naca 64a310(a=0 4) - Char , Moments & Ordinates Low-drag Pressure Distribution - Airfoils - Naca 64a010 Airfoils - Naca 64a910 - Char , Moments & Ordinates Low-drag Airfoils, Cambered Pressure Distribution - Airfoils Airfoils - Naca 64a310 - Char , Moments & Ordinates Low-drag 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 |