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Experimental evaluation of two 36 inch by 47 inch graphite/epoxy sandwich shear webs
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Bush, H. G. |
| Copyright Year | 1975 |
| Description | The design is described and test of two large (36 in. x 47 in.) graphite/epoxy sandwich shear webs. One sandwich web was designed to exhibit strength failure of the facings at a shear load of 7638 lbs/in., which is a characteristic loading for the space shuttle orbiter main engine thrust beam structure. The second sandwich web was designed to exhibit general instability failure at a shear load of 5000 lbs/in., to identify problem areas of stability critical sandwich webs and to assess the adequacy of contemporary analysis techniques. |
| File Size | 11035817 |
| Page Count | 55 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750025355 |
| Archival Resource Key | ark:/13960/t1ck35t3r |
| Language | English |
| Publisher Date | 1975-10-01 |
| Access Restriction | Open |
| Subject Keyword | Structural Mechanics Stress Analysis Composite Materials Epoxy Resins Graphite Failure Modes Shear Stress Sandwich Structures Loads Forces 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 |
