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![WADCTR53-334.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/97936db7ec26a8badd0fbc3dc2598e2f5b434cad.jpg)
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Calculating Cushion Thickness By Analysis Of Stress-Strain Curves
Author(s): Jones, R. E., Hunzicker, D. L.Corporate Author(s): Forest Products Laboratory, United States Department Of Agriculture
Laboratory: Materials Laboratory
Date of Publication: 1954-01
Report number: WADC TR 53-334
![AFFDLTR68-150article05.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/fd80af6a10e9b1986798fef6ee06ff0ca68cc728.jpg)
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Dynamic Analysis of Shells Using Double-Curved Finite Elements
Author(s): Greene, B. E., McLay, R. W., Strome, D. R., Jones, R. E.Corporate Author(s): University of California
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1969-12
Report number: AFFDL TR 68-150 p. 185-212
![WRDCTR89-3116volume03article25.pdf application/pdf thumbnail](https://digital2.library.iit.edu/files//medium/8172e74a1bbf7d3e76efab9baf68a4b991c3b5bc.jpg)
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Application of the Component Element Method to the Impact Damped Simple Harmonic Oscillation
Author(s): North, C. M., Jones, R. E.Corporate Author(s): Rose-Hulman Institute of Technology; Texas A&M University
Laboratory: Flight Dynamics Laboratory
Date of Publication: 1989-11
Report number: WRDC-TR-89-3116 Volume III p. KBA-1
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