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Sidewash in the vicinity of lifting swept wings at supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1957 |
| Description | Equations and charts have been presented for the conical part of the sidewash above and below swept wings at small angles of attack. This flow-field component is necessary in making calculations of the wing-induced forces and moments on stores, missiles, and pylons. All supersonic Mach numbers and wing leading-edge sweep angles have been considered. |
| File Size | 17228212 |
| Page Count | 51 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930084984 |
| Archival Resource Key | ark:/13960/t7vm9021g |
| Language | English |
| Publisher Date | 1957-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamic Loads, Bodies Wings, Complete - Wake Stores - Airplane Components Wings, Complete - Theory Flow, 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 |