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Tests of a triangular wing of aspect ratio 2 in the ames 12-foot pressure wind tunnel i : the effect of reynolds number and mach number on the aerodynamic characteristics of the wing with flap undeflected
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| File Size | 19691015 |
| Page Count | 43 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085772 |
| Archival Resource Key | ark:/13960/t3hx5p83s |
| Language | English |
| Publisher Date | 1948-01-22 |
| Access Restriction | Open |
| Subject Keyword | Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |