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A study of stall phenomena on a 45 degree swept-forward wing
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 15321552 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082472 |
| Archival Resource Key | ark:/13960/t5p88mj18 |
| Language | English |
| Publisher Date | 1949-01-27 |
| Access Restriction | Open |
| Subject Keyword | Airfoils - Naca 64a112 (a=0 8)(mod ) - Char & Ordinates Wings, Sweptforward - Characteristics Boundary Layer Separation - Wings, Sweptforward Wind Tunnel Tests - Aal - Full-scale (80'x40') Stalling - Sweptforward Wings Airfoils - Naca 641a112 - Low-drag Pitching Moments - Wings, Sweptforward Pressure Distribution - Wings, Sweptforward 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 |