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Charts for determining preliminary values of span-load, shear, bending-moment, and accumulated-torque distributions of swept wings of various taper ratios
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1948 |
| Description | Contains charts for use in determining preliminary values of the spanwise-load, shear, bending-moment, and accumulated-torque distributions of swept wings. The charts are based on strip theory and include four aerodynamic-load distributions, two section-moment distributions, and two inertia-load distributions. The taper ratios considered cover the range from 1.0 to 0 and the results are applicable to any angle of sweep. |
| File Size | 26051084 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930085396 |
| Archival Resource Key | ark:/13960/t7bs34880 |
| Language | English |
| Publisher Date | 1948-07-06 |
| Access Restriction | Open |
| Subject Keyword | Loads, Maneuvering - Wings Sweep - Complete Wings Taper - Complete Wings Loads, Steady Aerodynamic - 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 |