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Critical combinations of shear and direct axial stress for curved rectangular panels
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1949 |
| Description | A solution is presented for the problem of the buckling of curved rectangular panels subjected to combined shear and direct axial stress. Charts giving theoretical critical combinations of shear and direct axial stress are presented for panels having five different length-width ratios. Because the actual critical compressive stress of rectangular panels having substantial curvature is known to be much lower than the theoretical value, a semiempirical method of analysis of curved panels subjected to combined shear and direct axial stress is presented for use in design. (author |
| File Size | 776079 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19930082606 |
| Archival Resource Key | ark:/13960/t3615cb6n |
| Language | English |
| Publisher Date | 1949-08-01 |
| Access Restriction | Open |
| Subject Keyword | Plates - Stresses, Shearing Curved Plates - Compression Rectangular Plates - Buckling Rectangular Plates - Buckling Curved Plates - Compression Curved Stressed Skin - Plates Plates, Flat - Shear Rectangular 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 |