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Theoretical calculations of the effects of finite sideslip at supersonic speeds on the span loading and rolling moment for families of thin sweptback tapered wings at an angle of attack
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1953 |
| File Size | 1513046 |
| Page Count | 54 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930083688 |
| Archival Resource Key | ark:/13960/t2z365g34 |
| Language | English |
| Publisher Date | 1953-11-01 |
| Access Restriction | Open |
| Subject Keyword | Wings, Complete - Aspect Ratio Wings, Complete - Sweep Wings, Complete - Theory Wings, Complete - Taper AND Twist Flow, Supersonic Mach Number Effects - Complete Wings Loads, Steady - Wings Stability, Directional - Static Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |