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Resistance of a delta wing in a supersonic flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1951 |
| Description | The resistance of a delta wing at small angle of attack in supersonic conical flow with its leading edges within the Mach cone is calculated by a method that separates out the suction force. |
| File Size | 273660 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930093957 |
| Archival Resource Key | ark:/13960/t4xh3z18g |
| Language | English |
| Publisher Date | 1951-04-01 |
| Access Restriction | Open |
| Subject Keyword | Drag - Wings, Delta Theories - Wings, Supersonic 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 |