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Note on compressibility effects on downwash at the tail at subcritical speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1945 |
| File Size | 667411 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930092476 |
| Archival Resource Key | ark:/13960/t02z5jz42 |
| Language | English |
| Publisher Date | 1945-01-01 |
| Access Restriction | Open |
| Subject Keyword | Airplanes - North American P-51b Wind Tunnel Tests (amer ) Lift Coefficients Airplanes - Lockheed P-58 Wind Tunnel Tests (amer ) Load Distribution, Wing-span Tail Surfaces, Horizontal Downwash Angles - Effect OF Compressibility Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |