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Method for calculating downwash field due to lifting surfaces at subsonic and supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1951 |
| File Size | 1448159 |
| Page Count | 31 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082987 |
| Archival Resource Key | ark:/13960/t5dc2cg65 |
| Language | English |
| Publisher Date | 1951-04-01 |
| Access Restriction | Open |
| Subject Keyword | Flow, Supersonic Theories - Flow Wings, Complete - Wake Thin Theories - Airfoils Wings,complete - Theory Loads, Steady - Wings Wings, Complete - Sweep Downwash Linear Flow, Subsonic Theories - Wings 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 |