Loading...
Please wait, while we are loading the content...
Similar Documents
Effects of compressibility on maximum lift coefficients for six propeller airfoils
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1945 |
| File Size | 686948 |
| Page Count | 20 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092733 |
| Archival Resource Key | ark:/13960/t53f93768 |
| Language | English |
| Publisher Date | 1945-01-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution - Airfoils - Naca 16-515 Airfoils - Naca 16-515 - Characteristics Propeller Wind Tunnel Tests (naca-high-speed-8') Pressure Distritution - Airfoils - Naca 16-715 Airfoils - Naca 16-509 - Characteristics Propeller Airfoils, Cambered - Characteristics Airfoils - Naca 16-715 - Characteristics Propeller Airfoils - Naca16-709 - Characteristics Propeller Pressure Distribution - Airfoils - Naca 16-215 Airfoils - Naca 16-209 - Characteristics Propeller 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 |