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A flat wing with sharp edges in a supersonic stream
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1956 |
| Description | A basic treatment is given for the approximate solution of the problem of two-dimensional supersonic flow past a thin wing at small angles of attack. The pressure distribution at the surface, the lifting force, and the wave drag are determined. |
| File Size | 1372569 |
| Page Count | 49 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930093836 |
| Archival Resource Key | ark:/13960/t43r5ks6j |
| Language | English |
| Publisher Date | 1956-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics, Fundamental Aerodynamics Flow, Compressible Flow, Supersonic Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |