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Supersonic lift and pitching moment of thin sweptback tapered wings produced by constant vertical acceleration.subsonic leading edges and supersonic trailing edges
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1951 |
| File Size | 11525071 |
| Page Count | 45 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082993 |
| Archival Resource Key | ark:/13960/t5p88mm6k |
| Language | English |
| Publisher Date | 1951-03-01 |
| Access Restriction | Open |
| Subject Keyword | Pressure Distribution - Wings, Sweptback Wings, Thin Pitching Moments - Wings, Sweptback Wings - Aspect Ratio Wings, Sweptback - Characteristics Wings, Sweptback - Tapered Supersonic Effect OF Compressibility 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 |