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Comparison of theoretical stresses and deflections of multicell wings with experimental results obtained from plastic models
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1956 |
| Description | The experimental deflections and stresses of six plastic multicell-wing models of unswept, delta, and swept plan form are presented and compared with previously published theoretical results obtained by the electrical analog method. The comparisons indicate that the theory is reliable except for the evaluation of stresses in the vicinity of the leading edge of delta wings and the leading and trailing edges of swept wings. The stresses in these regions are questionable, apparently because of simplifications employed in idealizing the actual structure for theoretical purposes and because of local effects of concentrated loads. |
| File Size | 15615838 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930084614 |
| Archival Resource Key | ark:/13960/t2v45fr2k |
| Language | English |
| Publisher Date | 1956-11-01 |
| Access Restriction | Open |
| Subject Keyword | Loads AND Stresses, Structural - Torsion Loads AND Stresses, Structural - Bending Beams, Box Plastics Boxes, Structural 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 |
