Citation
Nagamatsu, Henry Takeshi (1940) Experimental Investigation of Ultimate Loads Carried by Flat, Unstiffened Panels Under Combined Shear and Compression. Master's thesis, California Institute of Technology. doi:10.7907/FNQF-4Q12. https://resolver.caltech.edu/CaltechETD:etd-11142008-140614
Abstract
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in .pdf document. The behavior of flat, unstiffened panels was investigated for two length over width ratios and five thicknesses. In each case the panels were loaded until they failed. An empirical relation was developed for the variation of the ultimate combined shear and compression stress of the form [...]. The values of m and n were found to be: m = 1.65 and n = .9 for panels with length over width ratio equal to 2, and m = 1.4 and n = 1.3 for panels with length over width ratio equal to 1 1/3. The above equations agree very closely with the experimental results. There was a variation in the apparent shear modulus under different combined loading conditions, but no definite result was obtained.
Item Type: | Thesis (Master's thesis) |
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Subject Keywords: | Aeronautics |
Degree Grantor: | California Institute of Technology |
Division: | Engineering and Applied Science |
Major Option: | Aeronautics |
Thesis Availability: | Public (worldwide access) |
Research Advisor(s): |
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Group: | GALCIT |
Thesis Committee: |
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Defense Date: | 1 January 1940 |
Record Number: | CaltechETD:etd-11142008-140614 |
Persistent URL: | https://resolver.caltech.edu/CaltechETD:etd-11142008-140614 |
DOI: | 10.7907/FNQF-4Q12 |
Default Usage Policy: | No commercial reproduction, distribution, display or performance rights in this work are provided. |
ID Code: | 4562 |
Collection: | CaltechTHESIS |
Deposited By: | Imported from ETD-db |
Deposited On: | 25 Nov 2008 |
Last Modified: | 20 Dec 2019 19:59 |
Thesis Files
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PDF (Nagamatsu_ht_1940.pdf)
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