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Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds subsonic leading edges and supersonic trailing edges
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| File Size | 1558488 |
| Page Count | 41 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082532 |
| Archival Resource Key | ark:/13960/t02z5k278 |
| Language | English |
| Publisher Date | 1949-04-01 |
| Access Restriction | Open |
| Subject Keyword | Damping IN Roll Theories - Wings, Supersonic Wings, Sweptback - Characteristics, Effect OF Compressibility Wings, Sweptback - Tapered Pressure Distribution - Wings, Sweptback Wings, Thin 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 |